Datos Sailplane
14
PARTES DEL AVION CANTIDAD n Ala 1 Fuselaje 1 Estabilizador Vertical 1 Estabilizador Horizontal 1 Tiempo Velocidad 0 0 1 8.90749572551118 2 16.2433618932192 3 22.2848952364682 4 27.2604665327741 5 31.3581530501027 6 34.7328478930373 7 37.5121149830815 8 39.8010109921458 9 41.686056498955 10 43.2385064786262 11 44.517043750366 12 45.5699971959734 13 46.4371685981084 14 47.15133715306 15 47.7394985287995 16 48.223885304881 17 48.6228073669556 18 48.9513440229254 19 49.2219140028221 20 49.4447448884813 21 49.6282597175198
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Transcript of Datos Sailplane
SUMA DE RESISTENCIA DEL PLANEADOR
PARTES DEL AVION
Ala 1Fuselaje 1Estabilizador Vertical 1Estabilizador Horizontal 1
RESISTENCIA TOTAL
Tiempo Velocidad0 01 8.907495725511182 16.24336189321923 22.28489523646824 27.26046653277415 31.35815305010276 34.73284789303737 37.51211498308158 39.80101099214589 41.68605649895510 43.238506478626211 44.51704375036612 45.569997195973413 46.437168598108414 47.1513371530615 47.739498528799516 48.22388530488117 48.622807366955618 48.951344022925419 49.221914002822120 49.444744888481321 49.6282597175198
CANTIDAD n
22 49.779395375296223 49.903864810116324 50.006372983451125 50.090794718117526 50.160321167104127 50.217580439586428 50.264736943808729 50.303573202008730 50.335557229999231 50.361898028364232 50.383591282844533 50.401457001393734 50.416170510589335 50.428287983068836 50.438267460931137 50.44648616978938 50.453254777949139 50.4588291397151
SUMA DE RESISTENCIA DEL PLANEADOR
0.48 0.00724 0.00347520.045 0.00591 0.000265950.055 0.00622 0.00034210.11 0.00622 0.0006842
RESISTENCIA TOTAL 0.00476745
grafica
AREA EN EL PLANO O SECCION MAXIMA Si
COEFICIENTE DE RESISTENCIA CDmin ηCDmin Si
CALCULO DE ALA
0.29 0 0.25 00.282 0.1 0.258 0.3875968992250.279 0.2 0.261 0.7662835249040.276 0.3 0.264 1.1363636363640.273 0.4 0.267 1.498127340824
0.27 0.5 0.27 1.8518518518520.267 0.6 0.273 2.1978021978020.264 0.7 0.276 2.5362318840580.261 0.8 0.279 2.8673835125450.258 0.9 0.29 3.103448275862
0.25
𝑍 ̅� 𝐶(𝑧) 𝐶_𝐶𝐴𝑀/(𝐶(𝑧))
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 10
0.5
1
1.5
2
2.5
3
0
0.449728682170543
0.897343550446999
1.33291666666667
1.73513108614232
2.07098765432099
2.304810744810742.414408212560392.38126642771804
2.03458620689655
COEFICIENTE DE SUSTENTACION DEL ALA
C(z)
CL M
AX
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 10
0.5
1
1.5
2
2.5
3
0
0.449728682170543
0.897343550446999
1.33291666666667
1.73513108614232
2.07098765432099
2.304810744810742.414408212560392.38126642771804
2.03458620689655
COEFICIENTE DE SUSTENTACION DEL ALA
C(z)
CL M
AX
CALCULO DE ALA
1.2003 -0.3 -0.053333333333 0.0096 0 0.0015079644741.2003 -0.225 -0.04 0.0096 0 0.0015079644741.1977 -0.15 -0.026666666667 0.0094 0 0.0014765485471.1863 -0.075 -0.013333333333 0.0088 0 0.0013823007681.1582 0 0 0.0072 0 0.0011309733551.1066 0.066 0.011733333333 0.0044 0 0.0006911503841.0286 0.113 0.020088888889 0 0 00.9269 0.141 0.025066666667 -0.0062 0 -0.0009738937230.8038 0.15 0.026666666667 -0.0134 0 -0.0021048670780.6355 0.113 0.020088888889 -0.0184 0 -0.002890265241
Γ_𝑃𝐿 Γ_𝜒 Γ_𝑧 𝜑^°=0 𝜑^°=9〖𝜑 ^° Γ〗_𝑍𝐶_(𝐿 𝑚𝑎𝑥)
Γ_(𝜒=45)
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 10
0.5
1
1.5
2
2.5
3
0
0.449728682170543
0.897343550446999
1.33291666666667
1.73513108614232
2.07098765432099
2.304810744810742.414408212560392.38126642771804
2.03458620689655
COEFICIENTE DE SUSTENTACION DEL ALA
C(z)
CL M
AX
0 1 2 3 4 5 60
0.2
0.4
0.6
0.8
1
1.2
00.1
0.20.3
0.40.5
0.60.7
0.80.9
1
CD
CL
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 10
0.5
1
1.5
2
2.5
3
0
0.449728682170543
0.897343550446999
1.33291666666667
1.73513108614232
2.07098765432099
2.304810744810742.414408212560392.38126642771804
2.03458620689655
COEFICIENTE DE SUSTENTACION DEL ALA
C(z)
CL M
AX
0 1 2 3 4 5 60
0.2
0.4
0.6
0.8
1
1.2
00.1
0.20.3
0.40.5
0.60.7
0.80.9
1
CD
CL
0 0.2 0.4 0.6 0.8 1 1.20
0.05
0.1
0.15
0.2
0.25
0
0.0940521470587181
0.144349228420807
0.171351286837119
0.185269093923164
0.191554294869478
0.193273932270688
0.192225836492372
0.189498477852745
0.185767662503613
0.181461039001884
COEFICIENTE DE SUSTENCION CL
EFIC
IEN
CIA
AERO
DIN
AMIC
A K
CALCULO DE ALA
0.002010619298 0.002513274123 0 2.420.002010619298 0.002513274123 0.449728682171 2.42 5.38102214944410.001968731396 0.002460914245 0.897343550447 2.42 2.6968489368364
0.00184306769 0.002303834613 1.332916666667 2.42 1.81556736480150.001507964474 0.001884955592 1.735131086142 2.42 1.39470730443790.000921533845 0.001151917306 2.070987654321 2.42 1.1685245901639
0 0 2.304810744811 2.42 1.0499777499947-0.001298524963 -0.001623156204 2.41440821256 2.42 1.0023160074632-0.002806489437 -0.003508111797 2.381266427718 2.42 1.0162659548848-0.003853686988 -0.004817108736 2.034586206897 2.42 1.189431045879
0 0.7839230234270.1 1.0632399485530.2 1.3855287083140.3 1.750789302710.4 2.1590217317410.5 2.6102259954060.6 3.1044020937060.7 3.6415500266420.8 4.2216697942120.9 4.844761396416
1 5.510824833256
𝜑^°=12 𝜑^°=15 𝐶_𝐿^𝐼 𝐶_(𝐿 max ∞ ) 𝐶_( max ∞ )𝐿 /(𝐶_𝐿 𝑖)
𝐶_𝐿 𝐶_𝐷 𝐾= _𝐶 𝐿/ _𝐶 𝐷
0 1 2 3 4 5 60
0.2
0.4
0.6
0.8
1
1.2
00.1
0.20.3
0.40.5
0.60.7
0.80.9
1
CD
CL
0 1 2 3 4 5 60
0.05
0.1
0.15
0.2
0.25
0
0.0940521470587181
0.144349228420807
0.171351286837119
0.185269093923164
0.191554294869478
0.193273932270688
0.192225836492372
0.1894984778527450.18576766250361
30.18146103900188
4
COEFICIENTE DE RESISTENCIA CD
EFIC
IEN
CIA
AERO
DIN
AMIC
A K
0 1 2 3 4 5 60
0.2
0.4
0.6
0.8
1
1.2
00.1
0.20.3
0.40.5
0.60.7
0.80.9
1
CD
CL
0 0.2 0.4 0.6 0.8 1 1.20
0.05
0.1
0.15
0.2
0.25
0
0.0940521470587181
0.144349228420807
0.171351286837119
0.185269093923164
0.191554294869478
0.193273932270688
0.192225836492372
0.189498477852745
0.185767662503613
0.181461039001884
COEFICIENTE DE SUSTENCION CL
EFIC
IEN
CIA
AERO
DIN
AMIC
A K
0 1 2 3 4 5 60
0.05
0.1
0.15
0.2
0.25
0
0.0940521470587181
0.144349228420807
0.171351286837119
0.185269093923164
0.191554294869478
0.193273932270688
0.192225836492372
0.1894984778527450.18576766250361
30.18146103900188
4
COEFICIENTE DE RESISTENCIA CD
EFIC
IEN
CIA
AERO
DIN
AMIC
A K
00.094052150.144349230.171351290.185269090.191554290.193273930.192225840.189498480.185767660.18146104
𝐾= _𝐶 𝐿/ _𝐶 𝐷
0 1 2 3 4 5 60
0.05
0.1
0.15
0.2
0.25
0
0.0940521470587181
0.144349228420807
0.171351286837119
0.185269093923164
0.191554294869478
0.193273932270688
0.192225836492372
0.1894984778527450.18576766250361
30.18146103900188
4
COEFICIENTE DE RESISTENCIA CD
EFIC
IEN
CIA
AERO
DIN
AMIC
A K
0 1 2 3 4 5 60
0.05
0.1
0.15
0.2
0.25
0
0.0940521470587181
0.144349228420807
0.171351286837119
0.185269093923164
0.191554294869478
0.193273932270688
0.192225836492372
0.1894984778527450.18576766250361
30.18146103900188
4
COEFICIENTE DE RESISTENCIA CD
EFIC
IEN
CIA
AERO
DIN
AMIC
A K
