(274314947) Annauniversity Aeronauticalengineering 6 8

8/10/2019 (274314947) Annauniversity Aeronauticalengineering 6 8

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ANNA UNIVERSITY CHENNAI : : CHENNAI - 600 025

REGULATION 2008 - CURRICULUM

B.E. AERONAUTICAL ENGINEERING

AFFILIATED INSTITUTIONS

SEMESTER VI(Applicable to the students admitted from the Academic year 2008 2009 onwards)

Code No. Co!"e T#$%e L T & C

THEORY

MG23! " rin c ip le s o f M an a #e m e n t 3 0 0 3A$23! % in it e $ le m e n t M e t ho d 3 0 0 3

A$232 $ & p e rim en ta l ' t re ss A n a lys is 3 0 0 3

A$233 in d u n n e l e c h n i* u e s 3 0 0 3

A$23+ ,i# h te m p e ra tu re m a t e ria ls 3 0 0 3

$lecti-e . 3 0 0 +&RACTICAL

A$23 Ae ro $ n # in e / a bo ra to ry 0 0 3 2A$23 A ir c ra f t 1 e s i# n " roe ct . 0 0 3 2

A$234 A ir f ra m e / a bo ra t o ry 0 0 3 2TOTAL '8 0 ( 25

SEMESTER VIICode No. Co!"e T#$%e L T & C

THEORY

G$2022 o ta l 5 u a lit y M an a #e m e n t 3 0 0 3A$2+0! A - ion ics 3 0 0 3

A$2+02 6 o m p u t a t io n a l % lu id 1 y n a mics 3 0 0 3A$2+03 7 ib ra t ion s A n d $ le m e n t s o f Ae ro e la s t ic it y 3 0 0 3

$lecti-e .. 3 0 0 3$lecti-e ... 3 0 0 3

&RACTICAL

A$2+0+ A ir c ra f t 1 e s i# n " ro e ct .. 0 0 3 2

A$2+0 A ir c ra f t ' ys te m s / a b o ra to ry 0 0 3 2

A$2+0 A - ion ics / a b o ra to ry 0 0 3 2A$2+04 .den tif ic a t io n o f " ro e ct o r 0 0 2 !

TOTAL '8 0 '' 25


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SEMESTER VIIICode No. Co!"e T#$%e L T & C

THEORY

A$2+! 6 o m po s ite M a t e ria ls A n d ' tru c t u re s 3 0 0 3

$lecti-e .7 3 0 0 3

$lecti-e 7 3 0 0 3&RACTICAL

A$2+2 6 o m p re h e n s io n A n d e c hn ic a l ' e mina r 0 0 3 2A$2+3 " roe ct o r 0 0 !2

TOTAL ( 0 '5 ')

LIST OF ELECTIVE COURSES

E%e*$#+e , I


A$202! h e o ry o f $ la s t ic it y 3 0 0 3A$2022 A ir c ra f t G e ne ra l $ n # in ee rin # A n d M a in te n a n ce

" ra c tic e s3 0 0 3

A$2023 'p a ce M e c h an ics 3 0 0 3A$202+ , ea t ran s f e r 3 0 0 3

E%e*$#+e", II III


A$202 , e lic op te r he o ry 3 0 0 3

A$202 .ndu s t ria l Ae rod y na mics 3 0 0 3

A$2024 A ir f ra m e M a in te n an c e an d e pa ir 3 0 0 3

A$2028 Ae ro $ n # in e M a in t en an c e a n d e pa ir 3 0 0 3A$2029 h e o ry o f " la t e s a n d ' h e lls 3 0 0 3

A$2030 % a ti# u e A n d % ra c tu re 3 0 0 3

E%e*$#+e" , IV V


A$203! , y pe rs o n ic A e ro d y n a mics 3 0 0 3

A$2032 $ & p e rim en ta l A e ro d y n a mics 3 0 0 3A$2033 o c e t s a n d M iss ile s 3 0 0 3

A$203+ ' t ru c tu ra l 1 y na mics 3 0 0 3

A$203 A ir ra f f ic 6 on t ro l a n d " la nn in # 3 0 0 3

A$203 " ro d u c t io n " la n n in # A n d 6 o n t ro l 3 0 0 3

A$2034 $n# in e ' ys te m s A n d 6 o n tro ls 3 0 0 3


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MG25' &RINCI&LES OF MANAGEMENT L T & C(6ommon to all :ranches) 0 0

UNIT I OVERVIE/ OF MANAGEMENT(1efinition Mana#ement ole of mana#ers $-olution of Mana#ement thou#ht ;r#ani


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AE25' FINITE ELEMENT METHOD L T & C 0 0

OBECTIVEo introduce the concept of numerical analysis of structural components

UNIT I INTRODUCTION 4e-iew of basic appro&imate methods of analyses 'tiffness and %le&ibility matri& forsimple cases Go-ernin# e*uation and con-er#ence criteria of finite element method=

UNIT II DISCRETE ELEMENTS '2:ar? %rame? beam elements Application to static? dynamic and stability analysis=

UNIT III CONTINUUM ELEMENTS '07arious types of 21elements Application to plane stress? plane strain and a&isymmetricproblems=

UNIT IV ISO&ARAMETRIC ELEMENTS '0

Applications to two and threedimensional problems=

UNIT V FIELD &ROBLEM (Applications to other field problems lie heat transfer and fluid flow=

TOTAL: 45 &ERIODSTE1T BOO!= irupathi==6 and Asho 1=:? D.ntroduction to %inite $lements in

$n#ineerin#E? "rentice ,all .ndia? hird $dition? 2003=REFERENCES!= eddy B=>= DAn .ntroduction to %inite $lement MethodE? McGraw,ill? 2000=2= Crishnamurthy? 6='=? D%inite $lement AnalysisE? ata McGraw,ill? 2000=3= :athe? C=B= and ilson? $=/=? D>umerical Methods in %inite $lements

AnalysisE? "rentice ,all of .ndia? !98=

AE252 E1&ERIMENTAL STRESS ANALYSIS L T & C 0 0

OBECTIVEo brin# awareness on e&perimental method of findin# the response of the structure todifferent types of load=

UNIT I MEASUREMENTS E1TENSOMETER'0"rinciples of measurements? Accuracy? 'ensiti-ity and ran#e of measurements=Mechanical? ;ptical Acoustical and $lectrical e&tensometers and their uses? Ad-anta#esand disad-anta#es=

UNIT II ELECTRICAL RESISTANCE STRAIN GAUGES'0"rinciple of operation and re*uirements? ypes and their uses? Materials forstrain #au#e= 6alibration and temperature compensation? cross sensiti-ity? osetteanalysis? heastone brid#e and potentiometer circuits for static and dynamicstrain measurements? strain indicators=


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UNIT III &HOTOELASTICITY'0wo dimensional photo elasticity? 6oncept of li#ht photoelastic effects? stress optic law?.nterpretation of frin#e pattern? 6ompensation and separation techni*ues? "hoto elasticmaterials= .ntroduction to three dimensional photo elasticity=

UNIT IV BRITTLE COATING AND MOIRE METHODS8.ntroduction to Moire techni*ues? brittle coatin# methods andholo#raphy=

UNIT V NON , DESTRUCTIVE TESTING)%undamentals of >1?adio#raphy? ultrasonic? ma#netic particle inspection?%luorescent penetrant techni*ue? $ddy current testin#? Acoustic $mission echni*ue=

TE1T BOOSTOTAL: 45 &ERIODS

!= 'rinath? /='=? a#ha-a? M==? /in#aiah? C=? Gara#esha? G=? "ant :=? andamachandra? C=? D$&perimental 'tress AnalysisE? ata McGraw,ill? >ew 1elhi?!98+=

REFERENCES!= 1ally? B==? and iley? =%=? D$&perimental 'tress AnalysisE? McGraw,ill .nc=? >ew

For? 200? .7 edition=2= ,etyenyi? M=? D,and boo of $&perimental 'tress AnalysisE? Bohn iley and 'ons

.nc=? >ew For? !942=3= "olloc A=A=? DAcoustic $mission in Acoustics and 7ibration "ro#ressE? $d= 'tephens

==:=? 6hapman and ,all? !993

AE25 /IND TUNNEL TECHNIUES L T & C 0 0

OBECTIVEo introduce the basic concepts of measurement of forces and moments on modelsdurin# the wind tunnel testin#=

UNIT I /IND TUNNELS'06lassification nondimensional numberstypes of similarities /ayout of open circuitand closed circuit subsonic wind tunnels desi#n parametersener#y ratio ,"

calculations= 6alibration=

UNIT II HIGH S&EED /IND TUNNELS'0:low down? in draft and induction tunnel layouts and their desi#n features? ransonic?supersonic and hypersonic tunnels? their peculiarities and calibration= ,elium and #untunnels? 'hoc tubes?

UNIT III /IND TUNNEL MEASUREMENTS'2"ressure?-elocity and temperature measurements %orce measurements types ofbalanceshree component and si& component balances calibration of measurin#instruments=


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UNIT IV FLO/ VISUALIATION 6'moe and uft #rid techni*ues 1ye inection special techni*ues ;ptical methodsof flow -isuali


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TE1T BOOS!= a= =? D%low and %racture at $le-ated emperaturesE? American 'ociety for Metals?

H'A? !98=2= ,ert


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AE256 AIRCRAFT DESIGN &ROECT , I L T & C0 0 2

OBECTIVE

o introduce and de-elop the basic concept of aircraft desi#n=

$ach student is assi#ned the desi#n of an Airplane (or ,elicopter or any other fli#ht-ehicle)? for #i-en preliminary specifications= he followin# are the assi#nments to be

carried outI

E1 & E R IM E N T S

!= 6omparati-e confi#uration study of different types ofairplanes2= 6omparati-e study on specification and performance details ofaircraft3= "reparation of comparati-e data sheets+= or sheet layout procedures= 6omparati-e #raphs preparation and selection of main parameters for thedesi#n

= "reliminary wei#ht estimations? selection of mainparameters?4= "ower plant selection? Aerofoil selection? in# tail and controlsurfaces8= "reparation of layouts of balance dia#ram and three -iewdrawin#s9= 1ra# estimation!0= 1etailed performance calculations and stability estimates

TOTAL: 60 &ERIODS

L IS T O F E U I& M E N T S

(for a batch of 30 students)

S%.No. N=9e o> $?e E7#9e$ =$#$;! $n#ineerin# 1rawin# :oard 30

2 $n#ineerin# 1rawin# .nstruments 30

3= 6omputers with suitable software 30

AE25) AIRFRAME LABORATORY L T & C0 0 2

OBECTIVE

o #i-e trainin# on ri-etin#? patchwor? weldin# and carpentry

LIST OF E1&ERIMENTSAircraft wood #luin#sin#le scarf ointAircraft wood #luin#double scarf oint'tudy on M.G? .G "/A'MA weldin# of aircraft componentselded sin#le double 7oints=%abric "atch repairi-eted patch repairs=ube bendin# and flarin#'heet metal formin#="reparation of #lass epo&y of composite laminates and

specimens= 1etermination of elastic constants of composite


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specimens=TOTAL: 45 &ERIODS


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L IS T O F E U I& M E N T(for a batch of 30 students)

S%.No. N=9e o> $?e E7#9e$ =$#$;Eew se-enMana#ement tools=

UNIT IV TM TOOLS(:enchmarin# easons to :enchmar? :enchmarin# "rocess? 5uality %unction1eployment (5%1) ,ouse of 5uality? 5%1 "rocess? :enefits? a#uchi 5uality /oss%unction? otal "roducti-e Maintenance ("M) 6oncept? .mpro-ement >eeds? %M$A

'ta#es of %M$A=


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UNIT V UALITY SYSTEMS (>eed for .'; 9000 and ;ther 5uality 'ystems? .'; 9000I2000 5uality 'ystem $lements? .mplementation of 5uality 'ystem? 1ocumentation? 5uality Auditin#? '!9+9? .'; !+000 6oncept? e*uirements and :enefits=

TE1T BOOTOTAL: 45 &ERIODS

!= 1ale ,=:esterfiled? et al=? Dotal 5uality Mana#ementE? "earson $ducation? .nc=

2003= (.ndian reprint 200+)= .':> 8!294020=

REFERENCES!= $-ans= B= = /indsay= ?M Dhe Mana#ement and 6ontrol of 5ualityE? (

th$dition)?

'outhestern (homson /earnin#)? 2002 (.':> 032+080)=2= %ei#enbaum=A=7= Dotal 5uality Mana#ementE? McGraw,ill? !99!=3= ;aland=B='= Dotal 5uality Mana#ementE? :utterworth ,cinemann /td=? ;&ford?

!989=+= >arayana 7= and 'reeni-asan? >='= D5uality Mana#ement 6oncepts and assE?

>ew A#e .nternational !99== Jeiri= Dotal 5uality Mana#ement for $n#ineersE? ood ,ead "ublishers? !99!=

AE240' AVIONICS L T & C 0 0

OBECTIVEo introduce the basic concepts of na-i#ation communication systems of aircraft=

UNIT I INTRODUCTION TO AVIONICS8>eed for A-ionics in ci-il and military aircraft and space systems .nte#rated A-ionicssystem ypical a-ionics sub systems 1esi#n approaches and recent ad-ances

Application echnolo#ies=

UNIT II &RINCI&LES OF DIGITAL SYSTEMS'01i#ital 6omputers 1i#ital number system number systems and codes%undamentalsof lo#ic and combinational lo#ic circuits 1i#ital arithmetic interfacin# with analo#uesystems Microprocessors Memories=

UNIT III DIGITAL AVIONICS ARCHITECTURE 8A-ionics system architecture salient features and applications of 1ata buses M./'1!3 :A.>6 +29A.>6 29=

UNIT IV FLIGHT DEC AND COC&ITS(6ontrol and display technolo#ies 6? /$1? /61? $/ and plasma panel ouchscreen 1irect -oice input (17.) 6i-il cocpit and military cocpit I M%1'? ,H1? M%C?,;A'

UNIT V AVIONICS SYSTEMS'06ommunication 'ystems >a-i#ation systems %li#ht control systems adarelectronic warfare Htility systems eliability and maintainability 6ertification=


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TOTAL: 45 &ERIODS


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TE1T BOOS!= Malcrno A="= and /each? 1="=? D1i#ital "rinciples and ApplicationE? ata McGraw,ill?

!990=2= Gaonar? ='=? DMicroprocessors Architecture "ro#rammin# and

ApplicationE? iley and 'ons /td=? >ew 1elhi? !990=

REFERENCES

!= Middleton? 1=,=? $d=? DA-ionics 'ystems? /on#man 'cientific andechnicalE? /on#man Group HC /td=? $n#land? !989=2= 'pitew 1elhi?

!993=

AE2402 COM&UTATIONAL FLUID DYNAMICS L T & C 0 0

OBECTIVEo study the flow of dynamic fluids by computational methods

UNIT I FUNDAMENTAL CONCE&TS '0.ntroduction :asic $*uations of %luid 1ynamics .ncompressible .n -iscid%lowsI 'ource? -orte& and doublet panel? methods liftin# flows o-er arbitrary bodies=Mathematical properties of %luid 1ynamics $*uations K $lliptic? "arabolic and,yperbolic e*uations ell posed problems discreti


14/38

TE1T BOO!= %letcher? 6=A=B=? D6omputational echni*ues for %luid 1ynamicsE? 7ols= . and ..?

'prin#er 7erla#? :erlin? !988=

REFERENCES!= Bohn %= endt ($ditor)? D6omputational %luid 1ynamics An .ntroductionE? 'prin#er

7erla#? :erlin? !9922= 6harles ,irsch? D>umerical 6omputation of .nternal and $&ternal %lowsE? 7ols= . and..= Bohn iley 'ons? >ew For? !988=

3= Claus A ,offmann and 'te-e = 6hian#= D6omputational %luid 1ynamics for$n#ineersE? 7ols= . .. $n#ineerin# $ducation 'ystem? "=;= :o& 20048? =ichita? C='=? 4208 !048 H'A? !993=

+= Anderson? Br=1=? D%undamentals of AerodynamicsE? McGraw,ill? 2000=

AE240 VIBRATIONS ELEMENTS OF AEROELASTICITY L T & C 0 0

OBECTIVE

o study the dynamic beha-iour of different aircraft components and the interactionamon# the aerodynamic? elastic and inertia forces

UNIT I BASIC NOTIONS8'imple harmonic motion erminolo#ies >ewtons /aw 1 Alemberts principle $ner#y Methods

UNIT II SINGLE DEGREE OF FREEDOM SYSTEMS'2%ree -ibrations 1amped -ibrations %orced 7ibrations? with and without dampin# support e&citation 7ibration measurin# instruments=

UNIT III MULTI DEGREES OF FREEDOM SYSTEMS'0wo de#rees of freedom systems 'tatic and 1ynamic couplin#s -ibration absorber"rincipal co ordinates? "rincipal modes and ortho#onal condition $i#en -alueproblems=

,amiltons principle /a#ran#ean e*uation and application 7ibration of elastic bodies7ibration of strin#s /on#itudinal? /ateral and orsional -ibrations=

UNIT IV A&&RO1IMATE METHODS5aylei#hs and ,ol


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REFERENCES!= :isplin#hoff =/=? Ashley , and ,offman =/=? DAeroelasticityE Addision esley

"ublication? >ew For? !983=2= se= %='=? Morse? .=%=? ,inle? ==? DMechanical 7ibrationsE? "rentice ,all? >ew

For? !98+=3= 'canlan =,= osenbaum =? D.ntroduction to the study of Aircraft 7ibration

%lutterE? Bohn iley and 'ons= >ew For? !982=

+= on#ue= := ,=? D"rinciples of 7ibrationE? ;&ford Hni-ersity "ress? 2000=

AE2404 AIRCRAFT DESIGN &ROECT , II L T & C0 0 2

OBECTIVE

o enhance the nowled#e in continuation of the desi#n #i-en in proect.

$ach student is assi#ned the wor in continuation of the desi#n proect .=he followin# assi#nments are to be carried out=

L IS T O F E 1 &E R IM E N T S

!= 7n dia#ram for the desi#n study2= Gust and maneu-erability en-elopes3= 6ritical loadin# performance and final 7n #raph calculation+= 'tructural desi#n study heory approach= /oad estimation of win#s= /oad estimation of fusela#e=4= :alancin# and Maneu-erin# loads on tail plane? Aileron and udder loads=8= 1etailed structural layouts9= 1esi#n of some components of win#s? fusela#e!0= "reparation of a detailed desi#n report with drawin#s=

LIST OF EUI&MENTS

(for a batch of 30 students)

TOTAL: 60 &ERIODS

S.No. I$e9" =$#$;

!= 1rawin# :oard 30

2= 1rawin# .nstrument 20

3= 6omputers and suitablesoftware

30

AE2405 AIRCRAFT SYSTEMS LABORATORY L T &C

0 0 2OBECTIVEo train the students D;> ,A>1E e&perience in maintenance of -arious air framesystems in aircraft and rectification of common sna#s=

L IS T O F E 1 &E R IM E N T S!= Aircraft DBacin# HpE procedure2= Aircraft D/e-ellin#E procedure3= 6ontrol 'ystem Di##in# checE procedure+= Aircraft D'ymmetry 6hecE procedure= D%low testE to assess of filter element clo##in#


16/38

= D"ressure estE o assess hydraulic $&ternalL.nternal /eaa#e4= D%unctional estE to adust operatin# pressure8= D"ressure estE procedure on fuel system components9= D:rae or*ue /oad estE on wheel brae units!0= Maintenance and rectification of sna#s in hydraulic and fuel systems=

TOTAL: 60 &ERIODS

L IS T O F E U I& M E N T S(for a batch of 30 students)S.No. I$e9" =$#$; E


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L IS T O F E U I& M E N T(for a batch of 30 students)

S.No. De$=#%" o> E7#9e$" =$#$; E


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AE245' COM&OSITE MATERIALS AND STRUCTURES L T & C 0 0

OBECTIVEo understand the fabrication? analysis and desi#n of composite materials structures=

UNIT I STRESS STRAIN RELATION8.ntroduction Ad-anta#es and application of composite materials? reinforcements andmatrices Generalised ,ooes /aw $lastic constants for anisotropic? orthotropic andisotropic materials=

UNIT II METHODS OF ANALYSIS'0Micro mechanics Mechanics of materials approach? elasticity approach to determinematerial properties Macro Mechanics 'tressstrain relations with respect to naturala&is? arbitrary a&is 1etermination of material properties= $&perimental characterioastrandeinhold 6ompany? >ew For !998=

2= Bones? =M=? DMechanics of 6omposite MaterialsE? McGraw,ill? Co#ausha /td=?oyo? !998? .. edition=

REFERENCES!= A#arwal? :=1=? and :routman? /=B=? DAnalysis and " e rf o rman ce of%ibre

6ompositesE? Bohn iley and sons= .nc=? >ew For? !99=2= /ubin? G=? D,andboo on Ad-anced "lastics and %ibre GlassE? 7on >ostrand

einhold 6o=? >ew For? !989=AE2452 COM&REHENSION AND TECHNICAL SEMINAR L T &

C(6ommon o All :ranches) 0 0 2

OBECTIVE

he obecti-e of comprehension is to pro-ide opportunity for the student to apply thenowled#e ac*uired durin# the earlier semesters to real life problems which he L shemay ha-e to face in future as an en#ineer= hile learnin# as how to sol-e the real lifeproblems? student will recei-e #uidance from the faculty and also re-iew -arious courseslearnt earlier=

TOTAL: 45 &ERIODS


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AE245 &ROECT /OR L T & C(6ommon to all :ranches) 0 0 '2 6

OBECTIVEhe obecti-e of the proect wor is to enable the students in con-enient #roups of notmore than + members on a proect in-ol-in# theoretical and e&perimental studies relatedto the branch of study= $-ery proect wor shall ha-e a #uide who is the member of thefaculty of the institution= 'i& periods per wee shall be allotted in the time table and this

time shall be utilia-iers theory? 't= 7enants theory? "randtls theory on torsion? he semi in-ersemethod and applications to shafts of circular? elliptical? e*uilateral trian#ular andrectan#ular sections=


20/38


!= imosheno? '=? and Goodier? =>=? Dheory of $lasticityE? McGraw,ill /td=? oyo?!990=


21/38

REFERENCES!= $nrico 7olterra B=,= 6aines? DAd-anced 'tren#th of MaterialsE? "rentice ,all >ew

Bersey? !99!=2= n#? 6==? DApplied $lasticityE? McGraw,ill 6o=? >ew For? !993=3= 'oolnioff? .='=? DMathematical heory of $lasticityE? McGraw,ill >ew For? !948=

AE2022 AIRCRAFT GENERAL ENGINEERING AND L T & CMAINTENANCE &RACTICES 0 0

OBECTIVEo teach the students about the basic concepts of aircraft #eneral en#ineerin# andmaintenance practices=

UNIT I AIRCRAFT GROUND HANDLING AND SU&&ORT EUI&MENT'0

Moorin#? acin#? le-elin# and towin# operations "reparation $*uipment precautions $n#ine startin# procedures "iston en#ine? turboprops and turboets $n#ine fire e&tin#uishin# Ground power unit=

UNIT II GROUND SERVICING OF VARIOUS SUB SYSTEMS8

Air conditionin# and pressuriew For? !993=

REFERENCES:!= A" Mechanics? Aircraft ,and :oo? % A A ,imalayan :oo ,ouse? >ew 1elhi?

!992= A" Mechanics? General ,and :oo? % A A ,imalayan :o ,ouse? >ew 1elhi? !99


22/38

AE202 S&ACE MECHANICS L T & C 0 0

OBECTIVEo study the basic concepts of orbital Mechanics with particular emphasis oninterplanetary traectories

UNIT I BASIC CONCE&TS

4he 'olar 'ystem eferences %rames and 6oordinate 'ystems he 6elestial'phere he $cliptic Motion of 7ernal $*uino& 'idereal ime 'olar ime 'tandard ime he $arths Atmosphere=

UNIT II THE GENERAL N-BODY &ROBLEM'0he many body "roblem /a#ran#e Bacobian .dentity he 6ircular estricted hree:ody "roblem /ibration "oints elati-e Motion in the >body "roblem wo :ody"roblem 'atellite ;rbits elations :etween "osition and ime ;rbital $lements=

UNIT III SATELLITE INECTION AND SATELLITE ORBIT &ERTURBATIONS'2

General Aspects of satellite .nections 'atellite ;rbit ransfer 7arious 6ases ;rbit1e-iations 1ue to .nection $rrors 'pecial and General "erturbations 6owellsMethod $nces Method Method of -ibrations of ;rbital $lements General"erturbations Approach=

UNIT IV INTER&LANETARY TRAECTORIES6wo 1imensional .nterplanetary raectories %ast .nterplanetary raectories hree1imensional .nterplanetary raectories /aunch if .nterplanetary 'pacecraft

raectory about the ar#et "lanet=

UNIT V BALLISTIC MISSILE TRAECTORIES AND MATERIALS'

he :oost "hase he :allistic "hase raectory Geometry ;ptimal %li#hts ime of%li#ht e entry "hase he "osition of the .mpact "oint .nfluence 6oefficients='pace $n-ironment "eculiarities $ffect of 'pace $n-ironment on the 'election of'pacecraft Material=

TOTAL: 45 &ERIODS

TE1T BOO!= 6ornelisse? B==? Docet "ropulsion and 'pace 1ynamicE? =,= %reeman 6o=?

!98+=REFERENCES

!= 'utton? G="=? Docet "ropulsion $lementsE? Bohn iley? !993=2= 7an de Camp? "=? D$lements of AstromechanicsE? "itman? !949=

3= "arer $==? DMaterials for Missiles and 'pacecraftE? McGraw,ill :oo 6o= .nc=?!982=

AE2024 HEAT TRANSFER L T & C 0 0

OBECTIVEo introduce the concepts of heat transfer to enable the students to desi#n componentssubected to thermal loadin#=


23/38

UNIT I HEAT CONDUCTION'':asic Modes of ,eat ransfer ;ne dimensional steady state heat conductionI6omposite Medium 6ritical thicness $ffect of -ariation of thermal 6onducti-ity $&tended 'urfaces Hnsteady state=,eat 6onductionI /umped 'ystem Analysis ,eat ransfer in 'emi infinite and infinitesolids Hse of ransient emperature charts Application of numerical techni*ues=

UNIT II CONVECTIVE HEAT TRANSFER'0.ntroduction %ree con-ection in atmosphere free con-ection on a -ertical flat plate $mpirical relation in free con-ection %orced con-ection /aminar and turbulentcon-ecti-e heat transfer analysis in flows between parallel plates? o-er a flat plate andin a circular pipe= $mpirical relations? application of numerical techni*ues in problemsol-in#=

UNIT III RADIATIVE HEAT TRANSFER8.ntroduction to "hysical mechanism adiation properties adiation shape factors

,eat e&chan#e between non blac bodies adiation shields=

UNIT IV HEAT E1CHANGERS86lassification emperature 1istribution ;-erall heat transfer coefficient?,eat$&chan#e Analysis /M1 Method and $>H Method=

UNIT V HEAT TRANSFER &ROBLEMS IN AEROS&ACE ENGINEERING8,i#h'peed flow ,eat ransfer? ,eat ransfer problems in #as turbinecombustion chambers ocet thrust chambers Aerodynamic heatin# Ablati-e heattransfer=

TOTAL: 45 &ERIODSTE1T BOOS!= Funus A= 6en#el=? D,eat ransfer A practical approachE? 'econd $dition? ata

McGraw,ill? 2002=2= .ncropera= %="=and 1ewitt=1="= D .ntroduction to ,eat ransferE? Bohn iley and 'ons

2002=REFERENCES

!= /ienhard? B=,=? DA ,eat ransfer e&t :ooE? "rentice ,all .nc=? !98!=2= ,olman? B="= D,eat ransferE? McGraw,ill :oo 6o=? .nc=? >ew For?

th$dn=? !99!=

3= 'achde-a? '=6=? D%undamentals of $n#ineerin# ,eat Mass ransferE? iley$astern /td=? >ew 1elhi? !98!=

+= Mathur? M= and 'harma? ="= DGas urbine and Bet and ocet "ropulsionE?'tandard "ublishers? >ew 1elhi !988=

AE2025 HELICO&TER THEORY L T & C 0 0

OBECTIVE:o present the basic ideas of e-olution? performance and associated stability problemsof helicopter=

UNIT I DEVELO&MENT OF ROTATING /ING AIRCRAFT6$-olution of helicopter,elicopter confi#urationsrotor arran#ementscompound,elicopter et rotorno tail rotor concepts

UNIT II DYNAMICS OF HOVERING FLIGHT

'2


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Actuator disc theory:lade $lement heoryideal twist .nduced profile power%i#ure ofmerithrust and power coefficientscalculation of dra#? tor*ue? powerGround effect inho-er $stimation of ho-er ceilin#=


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UNIT III DYNAMICS OF FOR/ARD FLIGHT '0%orward fli#ht performance"arasite dra# and "ower'tall limitationsflappin#cyclic"itch Autorotation in ho-er and in forward fli#ht1ead mans cur-e=

UNIT IV CLIMB AND DESCENT &ERFORMANCE (7ertical fli#htflow patterns surroundin# the rotor"ower re*uired in climb anddescent 1escent speed calculationsaeoff techni*ues=

UNIT V HELICO&TER STABILITY AND CONTROL 8rim'tatic stabilitydynamic stability"ilots controlotor control%li#ht control systemsand stability ar#umentation%lyin# *ualities=

TE1T BOO:TOTAL: 45 &ERIODS

!= Gessow A Myers G=6 DAerodynamics of ,elicopterE Mac Millan 6o? !984

REFERENCES:!= Gupta= / D,elicopter $n#ineerin#E? ,imalayan :oos? !992= 'aunders D1ynamics of ,elicopter fli#htE? Bohn iley? !943= >ewman= ' D%oundation of ,elicopter %li#htE ,alsted "ress? !99+

+= 'eddon= B D:asic ,elicopter AerodynamicsE A.AA education series? !990=

AE2026 INDUSTRIAL AERODYNAMICS L T & C 0 0

OBECTIVE:o familiari


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UNIT V FLO/ INDUCED VIBRATIONS '07orte& sheddin#? loc effects of eynolds number on wae formation in turbulent flows across wind #allopin#wae #allopin#alon# wind #allopin# of circular cablesoscillation of tall structures and launch -ehicles under wind loadsstall flutter=

TOTAL: 45 &EERIODSREFERENCES:

!= 'corer =' D$n-ironmental AerodynamicsE? $llis ,arwood /td? $n#land? !9482= 'o-ran? M(ed) DAerodynamic dra# mechanism of bluff bodies and road -ehiclesE?"lenum "ress? >=F? !948

3= 'achs " Dind %orces in $n#ineerin#E? "er#amon "ress? !988+= :le-ins =1 D%low .nduced 7ibrationsE? 7an >ostrand? !990= 6al-ert >=G Dind "ower "rinciplesE? 6harles Griffin 6o /ondon? !949

AE202) AIRFRAME MAINTENANCE AND RE&AIR L T & C 0 0

OBECTIVEo study the maintenance aspect of airframe systems and rectification of sna#s

UNIT I /ELDING IN AIRCRAFT STRUCTURAL COM&ONENTS'0$*uipments used in weldin# shop and their maintenance $nsurin# *uality welds eldin# i#s and fi&tures 'olderin# and bra


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!= C;$'? AC.>'? 1$/"? DAircraft Maintenance and epairE? McGraw,ill? >ewFor? !992=


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REFERENCES!= /AF $.,M$.? DAircraft epair ManualE? "alamar :oos? Mar*uette? !992=2= :.MM 1=B= :;GG$' ,=$=? DAircraft MaintenanceE? "itman "ublishin# corp= >ew

For? !9+0

AE2028 AERO ENGINE MAINTENANCE AND RE&AIR L T & C 0 0 OBECTIVEo study the basic concepts of the maintenance and repair of both piston and et aeroen#ines and the procedures followed for o-erhaul of aero en#ines=

UNIT I CLASSIFICATION OF &ISTON ENGINE COM&ONENTS5ypes of piston en#ines "rinciples of operation %unction of components Materialsused 1etails of startin# the en#ines 1etails of carburetion and inection systems forsmall and lar#e en#ines .#nition system components 'par plu# details $n#ineoperatin# conditions at -arious altitudes Maintenance and inspection chec to be

carried out=

UNIT II INS&ECTIONS OF &ISTON ENGINES8.nspection and maintenance and trouble shootin# .nspection of all en#inecomponents

1aily and routine checs ;-erhaul procedures 6ompression testin# of cylinders 'pecial inspection schedules $n#ine fuel? control and e&haust systems $n#ine mount and super char#er 6hecs and inspection procedures=

UNIT III OVERHAULING OF &ISTON ENGINES'0'ymptoms of failure %ault dia#nostics 6ase studies of different en#ine systems lIools and e*uipment re*uirements for -arious checs and ali#nment durin# o-erhaulin#

ools for inspection ools for safety and for -isual inspection Methodsandinstruments for non destructi-e testin# techni*ues $*uipment for replacement of partand their repair= $n#ine testin#I $n#ine testin# procedures and schedule preparation ;nline maintenance=UNIT IV CLASSIFICATION OF ET ENGINE COM&ONENTS'2

!2 ypes of et en#ines "rinciples of operation %unctions of components Materialsused 1etails of startin# and operatin# procedures Gas turbine en#ine inspection checs Hse of instruments for online maintenance 'pecial inspection procedures I%orei#n ;bect 1ama#e :lade dama#e etc=

Maintenance procedures of #as turbine en#ines rouble shootin# and rectificationprocedures 6omponent maintenance procedures 'ystems maintenance procedures=Gas turbine testin# procedures test schedule preparation 'tora#e of $n#ines "reser-ation and depreser-ation procedures=

UNIT V OVERHAUL &ROCEDURES'0$n#ine ;-erhaul procedures .nspections and cleanin# of components epairsschedules for o-erhaul :alancin# of Gas turbine components=rouble 'hootin# "rocedures for rectification 6ondition monitorin# of the en#ineon #round and at altitude en#ine health monitorin# and correcti-e methods=


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TOTAL: 45 &ERIODS


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TE1T BOO

!= C;$' ./1? DAircraft "ower plantsE? 4th

$dition McGraw ,ill? >ew For? !99+=

REFERENCES!= H:;M$6A? DGas urbine $n#inesE? he $n#lish :oo 'tore? >ew 1elhi? !993=2= H>.$1 $6,>;/;G.$' "A ,.>$F? Dhe Aircraft Gas turbine $n#ine

and its ;perationE? (latest edition) he $n#lish :oo 'tore? >ew 1elhi=

AE202( THEORY OF &LATES AND SHELLS L T & C 0 0

OBECTIVEo study the beha-iour of the plates and shells with different #eometry under -arioustypes of loads=

UNIT I CLASSICAL &LATE THEORY

6lassical "late heory Assumptions 1ifferential $*uation :oundary6onditions=

UNIT II &LATES OF VARIOUS SHADES'5>a-iers Method of 'olution for 'imply 'upported ectan#ular "lates /ea-ys Methodof 'olution for ectan#ular "lates under 1ifferent :oundary 6onditions= Go-ernin#$*uation 'olution for A&isymmetric loadin# Annular "lates "lates of other shapes=

UNIT III EIGEN VALUE ANALYSIS8

'tability and free 7ibration Analysis of ectan#ular"lates=

UNIT IV A&&RO1IMATE METHODS'0aylei#h it


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AE202 E1&ERIMENTAL AERODYNAMICS L T & C 0 0

OBECTIVES:o present the measurement techni*ues in-ol-ed in aerodynamic testin#=

UNIT I /IND TUNNEL TESTING8

/ow speed wind tunnelsestimation of ener#y ratio and power re*uired supersonicwin tunnelscalculation of runnin# time and stora#e tan re*uirements=

UNIT II E1&ERIMENTS IN SUBSONIC /IND TUNNELS'0

$stimation of flow an#ularity and turbulence factorcalculation of 6/ and 61 on aero foilsfrom pressure distribution 61 from wae sur-eyest section a-era#e -elocity usin#tra-ersin# raesspan wise load distribution for different taper ratios of win#

UNIT III E1&ERIMENTS IN HIGH S&EED TUNNELS'0Mach number estimation in test section by pressure measurement and usin# a wed#e preliminary estimates of blowin# and runnin# pressures? no


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UNIT III VISCOUS HY&ERSONIC FLO/ THEORY (:oundary layer e*uation for hypersonic flowhypersonic boundary layersself similarand non self similar boundary layerssolution methods for non self similar boundarylayers aerodynamic heatin#=

UNIT IV VISCOUS INTERACTIONS IN HY&ERSONIC FLO/S (.ntroduction to the concept of -iscous interaction in hypersonic flowsstron# and wea

-iscous interactionshypersonic -iscous interaction similarity parameterintroduction toshoc wa-e boundary layer interactions=

UNIT V INTRODUCTION TO HIGH TEM&ERATURE EFFECTS (>ature of hi#h temperature flowschemical effects in airreal and perfect #asesGibbsfree ener#y and entropychemically reactin# mi&turesrecombination and dissociation=

TOTAL: 45 &ERIODSTE1T BOOS:!= Bohn= 1= Anderson= Br=? D,ypersonic and ,i#h emperature Gas 1yanmicsE? Mc=

Graw hill 'eries? >ew For? !99=

REFERENCES:

!= Bohn= 1= Anderson= Br =? DModern compressible flow with historical perspecti-eE? Mc=Graw ,ill "ublishin# 6ompany? >ew For? !99=O

2= Bohn= :ertin? D,ypersonic AerothermodynamicsE? published by A.AA.nc=? ashin#ton= 1=6=? !99+=

AE20 ROCETS AND MISSILES L T & C 0 0

OBECTIVEo introduce basic concepts of desi#n and traectory estimation of rocet and missiles

UNIT I ROCET MOTION IN FREE S&ACE AND GRAVITATIONAL FIELD

'0;ne 1imensional and wo 1imensional rocet Motions in %ree 'pace and,omo#eneous Gra-itational %ields description of 7ertical? .nclined and Gra-ity urnraectories 1etermination of ran#e and Altitude 'imple Appro&imations to :urnout7elocity=

UNIT II STAGING AND CONTROL OF ROCETS AND MISSILES'0Multista#in# of rocets 7ehicle ;ptimi


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UNIT V MATERIALS FOR ROCETS AND MISSILES 5'election of Materials 'pecial e*uirements of Materials to "erform under Ad-erse6onditions=

TE1T BOOSTOTAL: 45 &ERIODS

!= 'utton? G="=? et al=? Docet "ropulsion $lementsE? Bohn iley 'ons .nc=? >ew

For? !993=

REFERENCES!= Mathur? M=? and 'harma? ="=? DGas urbines and Bet and ocet "ropulsionE?

'tandard "ublishers? >ew 1elhi !998=2= 6ornelisse? B==? Docet "ropulsion and 'pace 1ynamicsE? B==? %reeman 6o=

/td=? /ondon? !982=3= "arer? $==? DMaterials for Missiles and 'pacecraftE? McGraw,ill :oo 6o= .nc=?

!982=

AE200 FATIGUE AND FRACTURE L T & C 0 0

OBECTIVEo study the concepts of estimation of the endurance and failure mechanism ofcomponents

UNIT I FATIGUE OF STRUCTURES 8'=>= cur-es $ndurance limits $ffect of mean stress? Goodman? Gerber and'oderber# relations and dia#rams >otches and stress concentrations >eubersstress concent rat ion factors "lastic stress concentration factors >otched '=>=cur-es=

UNIT II STATISTICAL AS&ECTS OF FATIGUE BEHAVIOUR (/ow cycle and hi#h cycle fati#ue 6offin Mansons relation ransition life cyclicstrain hardenin# and softenin# Analysis of load histories 6ycle countin# techni*ues 6umulati-e dama#e Miners theory ;ther theories=

UNIT III &HYSICAL AS&ECTS OF FATIGUE AND FRACTURE'2"hase in fati#ue life 6rac initiation 6rac #rowth %inal %racture 1islocations fati#ue fracture surfaces 'tren#th and stress analysis of craced bodies "otentialener#y and surface ener#y Griffiths theory .rwin ;rwin e &ten sion of Griffithstheory to ductile materials $ffect of thicness on fracture tou#hness stress intensityfactors for typical #eometries=

UNIT IV FATIGUE DESIGN ANDTESTINIG8

'afe life and %ailsafe desi#n philosophies .mportance of %racture Mechanics inaerospace structures Application to composite materials and structures=

UNIT V FUNDAMENTALS OF FAILURE ANALYSIS86ommon causes of failure= "rinciples of failure analysis= %racture mechanics approachto failure problems= echni*ues of failure analysis= 'er-ice failure mechanisms ductileand brittle fracture? fati#ue fracture? wear failures? frettin# failures? en-ironment inducedfailures? hi#h temp= failure= %aulty heat treatment and desi#n failures? processin# failures(for#in#? castin#? machinin# etc=)?

TOTAL: 45 &ERIODS


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TE1T BOOS!= "rasanth Cumar D$lements of fracture mechanicsE heeter publication?!999=2= :arrois ? ipely? $=/=? D%ati#ue of aircraft structureE? "eL#amon press= ;&ford?!983=

REFERENCES

!= 'in? 6=G=? DMechanics of fractureE 7ol= .? 'ithoff and w >oordhoff .nternational"ublishin# 6o=? >etherlands? !989=2= Cnott? B=%=? D%undamentals of %racture MechanicsE? :uterworth 6o=? /td=? /ondon?

!9833= 'ubra suresh? D%ati#ue of materialsE ? .. edition?!998=+= = /= Anderson? D%racture mechanicsI %undamentals and applicationsE? ... edition?

200+=

AE204 STRUCTURAL DYNAMICS L T &

C 0 0 UNIT I FORCE DEFLECTION &RO&ERTIES OF STRUCTURES(6onstraints and Generaliatural -ibrations of plates=

UNIT V A&&RO1IMATE METHODS(

Appro&imate methods of e-aluatin# the $i#en fre*uencies and the dynamics responseof continuous systemsMatri& methods of dynamic stress analysis=

TE1T BOOS:TOTAL: 45 &ERIODS

!= %= '= se? .= $= Morse and ,= = ,inle? DMechanical 7ibrationE? "rentice ,all of .ndia"-t= /td? >ew 1elhi? !988=

2= = 6= ,urty and M= %= ubinstein? D1ynamics of 'tructuresE? "rentice ,all of .ndia"-t= /td? >ew 1elhi? !984=

REFERENCES:!= = C= 7ierc? D7ibration AnalysisE 2

nd$dition? homas F= 6rowell 6o ,arper ow

"ublishers? >ew For? H='=A= !989=


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2= '= "= imoshno ad 1= ,= Foun#? D7inration "roblems in $n#ineerin#E? Bohn illey 'ons .nc=? !98+=

3= -on Carman and A= :iot? DMathematical Methods in $n#ineerin#E? McGraw,ill :oo6o=? >ew For? !98=


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AE205 AIR TRAFFIC CONTROL AND &LANNING L T & C 0 0

OBECTIVEo study the procedure of the formation of aerodrome and its desi#n and air trafficcontrol=

UNIT I BASIC CONCE&TS

(;becti-es of A' "arts of A6 ser-ice 'cope and "ro-ision of A6s 7% .%operations 6lassification of A' air spaces 7aries inds of separation Altimetersettin# procedures $stablishment? desi#nation and identification of units pro-idin#

A' 1i-ision of responsibility of control=

UNIT II AIR TRAFFIC SERVICES(

Area control ser-ice? assi#nment of cruisin# le-els minimum fli#ht altitude A' routesand si#nificant points >A7 and >" 7ertical? lateral and lon#itudinal separationsbased on time L distance A6 clearances %li#ht plans position report

UNIT III FLIGHT INFORMATION ALERTING SERVICES COORDINATIONEMERGENCY &ROCEDURES AND RULES OF THE AIR'0

adar ser-ice? :asic radar terminolo#y .dentification procedures usin# primary Lsecondary radar performance checs use of radar in area and approach controlser-ices assurance control and coordination between radar L non radar control emer#encies %li#ht information and ad-isory ser-ice Alertin# ser-ice 6oordinationand emer#ency procedures ules of the air=

UNIT IV AERODROME DATA &HYSICALCHARACTERISTICS

AND OBSTACLE RESTRICTION (Aerodrome data :asic terminolo#y Aerodrome reference code Aerodromereference point Aerodrome ele-ation Aerodrome reference temperature .nstrumentrunway? physical 6haracteristics len#th of primary L secondary runway idth ofrunways Minimum distance between parallel runways etc= obstacles restriction=

UNIT V VISUAL AIDS FOR NAVIGATION VISUAL AIDSFOR

DENOTING OBSTACLES EMERGENCY AND OTHER SERVICES 87isual aids for na-i#ation ind direction indicator /andin# direction indicator /ocation and characteristics of si#nal area Marin#s? #eneral re*uirements 7ariousmarin#s /i#hts? #eneral re*uirements Aerodrome beacon? identification beacon 'imple approach li#htin# system and -arious li#htin# systems 7A'. "A". 7isualaids for denotin# obstacles obect to be mared and li#hter $mer#ency and other

ser-ices=


!= A." (.ndia) 7ol= . ..? Dhe $n#lish :oo 'toreE? !4!? 6onnau#ht 6ircus? >ew 1elhi=

REFERENCES!= DAircraft Manual (.ndia) 7olume .E? latest $dition he $n#lish :oo 'tore? !4!?

6onnau#ht 6ircus? >ew 1elhi=2= D"A>' A6 .6A; 1;6 ++++E? /atest $dition? he $n#lish :oo 'tore? !4!?

6onnau#ht 6ircus? >ew 1elhi=


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AE206 &RODUCTION &LANNING AND CONTROL L T & C 0 0

OBECTIVE:o understand the -arious components and functions of production plannin# and controlsuch as product plannin#? product schedulin# and in-entory control=

UNIT I INTRODUCTION:8%actors affectin# plannin#%orecastin# information necessary for preplannin#sourcesof informationMethods of forecastin#aircraft components re*uirin# o-erhaulrepairmodificationsprematurefailuresproect plannin#estimates of plant? machinery?buildin#s? manpower? materials? spare parts? time? and cost estimates=

UNIT II MATERIALS MACHINES AND &ROCESSES:("roduction en#ineerin# nowled#e necessary for "lannin#? machine tools andprocesses=Materials includin# aircraft materials and their processin#'pare partsre*uired for o-erhaul and maintenanceGround handlin# e*uipmenttestin# ofcomponents and aircraft o-erhaulstandards for acceptance after o-erhaul=

UNIT III EUI&MENT AND TOOLS:'0"replannin# re*uired for pro-ision of special tools? i#s? fi&tures and test e*uipmentre*uired for o-erhaul and maintenancetypes and description of maor test e*uipment=

UNIT IV &RODUCTION &LANNING:'0"roduction plannin# function of routin#? estimatin# and schedulin# /;:6"M and"$= 5ueuin# theory? se*uencin# in obs? shop schedulin#? assembly line balancin#charts and #raphs=

UNIT V &RODUCTION CONTROL:8"roduction control functions of dispatchin#? pro#ressin# and e-aluationActi-ities ofpro#ressin#shop proceduresmaintenance of critical data statistics of e-aluation controlcharts=

TE1T BOOS:TOTAL: 45 &ERIODS

!= homas= /= D"roduction plannin# and controlE Mc Graw ,ill? !98=2= Bain= C= 6= and A##arwal= /= >= D"roduction plannin# and control and .ndustrial

Mana#ement? Channa publishers? !990=

REFERENCES:

!= :uffa= $= '= and 'arin= = C= DModern production L operations mana#ementE8th ed?Bohn illey and sons? 2000=

2= Mac>iece= $= ,= D"roduction forecastin#? plannin# and controlE? Bohn illey? !98=3= Ma#es= B= %= D"roduction plannin# and .n-entory controlE? McGraw ,ill? !990=


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AE 20) ENGINE SYSTEM AND CONTROL L T & C 0 0

OBECTIVE

o #i-e an e&posure to the different systems in Aircraft $n#ines and themethodolo#ies as well as instruments used for en#ine controls

indication=UNIT I ENGINE CONSTRUCTION'0/ayout "iston $n#ine urbo "ropGas urbine $n#ines Modular concept= ;il'ystem %uel systems ,eat Mana#ement system of Gas urbine $n#ines= /ubricantsand %uel used $n#ine Materials 6ompressor? urbine? %rames and 6astin# etc=

UNIT II ENGINE SYSTEMS(

Air 'ystem and "neumatics $n#ine controls %A1$6 %ire "rotection 'ystem .#nition and 'tartin# system $n#ine Antiicin# system=

UNIT III MAINTENANCE INS&ECTION6Maintenance aspects of Gas urbine $n#ines "re-enti-e condition(performance) Monitorin# :oroscopic .nspection ;n win# rim :alance estbed o-erhaul=

UNIT IV CONTROL INSTRUMENTS'0$n#ine sensors :asic construction "rocessin# si#nals Analo# and1i#ital.ndication 'calin# Monitorin# of .nstruments L.ndicators=

UNIT V ENGINE INSTRUMENTS'0"rimary instruments "M? %uel flow? $&haust Gas emperature? hrust parameters

'econdary .nstruments 7ibration indicator? ;il "ressure and ;il emperatureindictor? >acelle emp= .ndicator=

TE1T BOOS!= Aircraft .nstruments $ , B "allett? "itman 6o=? !993

TOTAL: 45 &ERIODS

2= Aircraft Gas urbine $n#ine echnolo#y .rwin $ rea#er? $n#lish :oo'tores? >ew 1elhi

3= Aircraft Gas urbine and ;peration "A A>1 ,.$>F? Hnitedechnolo#ies? $n#lish :oo 'tores? >ew 1elhi

REFERENCES!= DGeneral ,and :oo of Airframe and "ower "lantE H' 1epartment of

ransportation? %AA? $n#lish :oo 'tores? >ew 1elhi2= urbo Mache of Gas urbine? $n#lish :oo 'tores? >ew 1elhi3= Aircraft Gas urbine Guide? " "ublications? $n#lish :oo 'tores? >ew 1elhi+= olls oyce? he Bet $n#ine? olls oyce /td=? ... $dition? !983

(274314947) Annauniversity Aeronauticalengineering 6 8

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Transcript of (274314947) Annauniversity Aeronauticalengineering 6 8