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NARI Fluorescence-Doped Particles for Simultaneous Temperature and Velocity Imaging Principle Investigators: P. M. Danehy, P. Tiemsin, C. Wohl, (NASA Langley Research Center) Additional Team Members: T. Lowe and R. Simpson (Va Tech) NASA Aeronautics Mission Directorate FY11 Seedling Phase I Technical Seminar

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NARI

Fluorescence-Doped Particles for Simultaneous Temperature

and Velocity ImagingPrinciple Investigators:

P. M. Danehy, P. Tiemsin, C. Wohl, (NASA Langley Research Center)

Additional Team Members:T. Lowe and R. Simpson (Va Tech)

NASA Aeronautics Mission Directorate FY11 Seedling Phase I Technical Seminar

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Outline

• Current state of the art• Technical approach• The innovation: key points• Impact of the innovation if it is eventually

implemented• Results of the seedling Phase I effort to date• Distribution/Dissemination – getting the word out

• Next steps

June 5-7, 2012 NASA Aeronautics Mission Directorate FY11 Seedling Phase I Technical Seminar 2

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Current state of the art

• Most common measurements in wind tunnels are lift, drag, force and moment– Also: surface pressure, surface heat transfer

• Off body, most common techniques:– Schlieren, non-quantitative flow vis– Laser Doppler velocimetry (LDV), u, v at a point– Particle Image Velocimetry (PIV), u, v in a plane

• Measurements not readily available:– In stream temperature, pressure, concentration

June 5-7, 2012 NASA Aeronautics Mission Directorate FY11 Seedling Phase I Technical Seminar 3Need: Easy to use, turn key, safe

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Why Use Particles?• Other ways of measuring flow temperature (without seeding

particles) exist, but have limitations preventing their use:– CARS: complicated, expensive, hard to set up, single point, 10 Hz– Rayleigh/Raman scattering: low signal, complicated to analyze, often

single point, 10 Hz– PLIF: must seed flow with (usually) toxic gas, complicated, not very

accurate, not sensitive enough, 10 Hz– Thermocouple: intrusive probe, single point, slow time response

• Few or no viable methods of measuring flow pressure exist• Seeding dye-doped particles into a flow to measure T, P, and/or

stream concentration should allow high s/n images– Easy because uses same or similar lasers, seeding systems, detectors as

PIV/LDV prefer imaging, non-toxic seeding– Performing in conjunction with PIV/LDV will measure multi-parameters

June 5-7, 2012 NASA Aeronautics Mission Directorate FY11 Seedling Phase I Technical Seminar 4

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Technical Approach: Measure T

June 5-7, 2012 NASA Aeronautics Mission Directorate FY11 Seedling Phase I Technical Seminar 5

Laser

Dye-doped Particles

Mie Scattering

Fluorescence

LIFMIE

Temperature

If dye has T dependence…

Temperature (only) Measurement Approach

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Technical Approach: Measure P

June 5-7, 2012 NASA Aeronautics Mission Directorate FY11 Seedling Phase I Technical Seminar 6

Laser

Fluorescence

LIF

Time

Dye fluorescence lifetime depends on pressure…

Pressure (only) Measurement Approach using Lifetime Measurement(could also measure intensity of signal referenced to Mie)

P1P2

Dye-doped Particles

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Technical Approach: Combine w’ LDV

June 5-7, 2012 NASA Aeronautics Mission Directorate FY11 Seedling Phase I Technical Seminar 7

Laser

Fluorescence

DET1

Time

Measure velocity from frequency of collected light from particle passing through fringes…

Measure velocity from LDV, Pressure or Temperature from fluorescence

Mie Scattering

Dye-doped Particles

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Technical Approach: Imaging Example

June 5-7, 2012 NASA Aeronautics Mission Directorate FY11 Seedling Phase I Technical Seminar 8

Combine T, P or concentration measurement with Particle Image Velocimetry (PIV)

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Technical Approach: PSLs

Mg2+

Styrene

Mg2+

Mg2+

Mg2+

Mg2+

Mg2+

Mg2+

Mg2+

Mg2+

Styrene

S2O82-

Negatively charged monomer liquid

droplet

Magnesium cations neutralize negative

charge

Charge neutralization enables polymerization initiation by

persulfate radical

Polystyrene Latex Spheres

(PSLs)

June 5-7, 2012 NASA Aeronautics Mission Directorate FY11 Seedling Phase I Technical Seminar 9

Dye-

How do we attach the dye?

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Technical Approach: Dye Doping

A B C

Dye- Styrene- Premature Particle-

Mature Particle-

D

Dye with a Styrene functionality-June 5-7, 2012 NASA Aeronautics Mission Directorate FY11 Seedling Phase I Technical Seminar 10

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Technical Approach: Dye Doping

A B C

Dye- Styrene- Premature Particle-

Mature Particle-

D

Dye with a Styrene functionality-June 5-7, 2012 NASA Aeronautics Mission Directorate FY11 Seedling Phase I Technical Seminar 11

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Innovation: Key Points• Have identified multiple measurement approaches

with different dyes and different laser and detector configurations to measure:– Temperature, Pressure, Concentration– Pointwise (fast) or imaging (10 Hz) are possible– Alone or simultaneous with LDV, PIV

• PSLs have been synthesized with an array of dye materials with varying degrees of success– Dye influence on particle size and size distribution was

observed and characterized– Different methods of incorporating dyes explored

• Temperature measurement in a flow experiment was demonstrated with (VT, POC: Todd Lowe)

June 5-7, 2012 NASA Aeronautics Mission Directorate FY11 Seedling Phase I Technical Seminar 12

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Impact of Innovation if Incorporated

• Extend measurement technology beyond force/moment/wall and u, v velocity measurements– Temperature, Pressure, Concentration

• Impact on NASA ARMD Programs:– SFW/ERA: Jet noise studies, T, u, v and correlations– Rotary Wing: Pressure disturbances near blade tips– High Speed: Sonic Boom simultaneous P, u, v measurement– Measurements would provide unique data for validating

CFD codes in a way not currently possible.

• Have identified potential customers within NASA, at other government agencies, academia and industry.

June 5-7, 2012 NASA Aeronautics Mission Directorate FY11 Seedling Phase I Technical Seminar 13

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Phase I Results

June 5-7, 2012 NASA Aeronautics Mission Directorate FY11 Seedling Phase I Technical Seminar 14

Dye λexc, nm λem, nm PSL Incorporation notes

Rhodamine B 575 595 Great, no leaching Potentially carcinogenic

Fluorescein 548 512 526 Solvent dependent emission Non-carcinogenic

Kiton Red 620 554 575 Leaching issues Non-carcinogenic

Tetraphenyl Porphyrin 400 655 Inefficient incorporation Tunable spectral properties

• Dye materials evaluated

Other materials evaluted including fluorenone, 4-hydroxycoumarin, and Malachite Green.

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Phase I Results: Rh B

• Spectrum shifts in PSLs: Excitation and emission properties of Rhodamine dyes are strongly dependent on matrix properties

• Decreases particle size ~10%

0

0.2

0.4

0.6

0.8

1

1.2

500 550 600 650 700

Inte

nsity

, a.u

.

Wavelength, nm

In WaterIn PSLs

In Water In PSLs

Excitation Maximum

546 nm 575 nm

Emission Maximum

585 nm 595 nm

June 5-7, 2012 NASA Aeronautics Mission Directorate FY11 Seedling Phase I Technical Seminar 15

• Rhodamine B: Very strong Signal - But slightly toxic

O(Et)2N N+

CO2H

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Phase I Results: FL548

• Fluorescein 548 – Showed good signal and temperature sensitivity in preliminary tests– Shows Complex Emission/Quantum Yield Behavior

June 5-7, 2012 NASA Aeronautics Mission Directorate FY11 Seedling Phase I Technical Seminar 16

O

COOH

O

ClCl

HO

• Excitation at 532 nm.• Emission intensity

diminishes significantly and rapidly as solution evaporated.

• No detectable signal after the deposited PSLs were allowed to dry.

0

5

10

15

20

25

30

35

40

45

50

500 550 600 650 700 750 800

Fluo

resc

ent E

mis

sion

Inte

nsity

, a.u

.

Wavelength, nm

Have obtained a different type of Fluorescein dye that emits even when dry: will try soon.

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Phase I Results: KR

• Kiton Red – Less Toxic than Rh B– Lower signal than Rh B– Better for concentration meas.– Dye Leaching out:

June 5-7, 2012 NASA Aeronautics Mission Directorate FY11 Seedling Phase I Technical Seminar 17

O(Et)2N N+

SO3-

SO3-Na+

• Once PSLs have settled, there is a clear distinction in color between the PSLs (white) and aqueous solution (red).

0

50

100

150

200

250

500 600 700 800

Fluo

resc

ent E

mis

sion

Inte

nsity

, a.u

.

Wavelength, nm

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Phase I Results: Leaching

June 5-7, 2012 NASA Aeronautics Mission Directorate FY11 Seedling Phase I Technical Seminar 18

Rhodamine B-doped PSLs Kiton Red-doped PSLs

Even if Rh B is slightly toxic, if it is encapsulated in a polymer and won’t leach out (in water), might it be acceptable for use?

• Leaching Studies

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Phase I Results: PorphyrinPorphyrin-Suitable for pressure measurement-So far, low signal intensity

Complex Spectroscopic Properties:

• Coordination of an ion in the center of the macrocycle impacts:– Fluorescent emission– Quantum yield– Phosphorescent properties– Propensity for PSL incorporation?

• PSL synthesis uses MgSO4 resulting in formation of a Mg-TPP adduct: Chlorophyll-like

Fluorescent Emission

June 5-7, 2012 NASA Aeronautics Mission Directorate FY11 Seedling Phase I Technical Seminar 19

0

10

20

30

40

50

60

70

80

90

100

350 450 550 650 750

Emis

sion

Inte

nsity

, a.u

.

Wavelength, nm

λmax: 655 nm

HN

NNH

N N

NN

NMg+2

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Phase I Results: Concept Demo I

June 5-7, 2012 NASA Aeronautics Mission Directorate FY11 Seedling Phase I Technical Seminar 20

532 nmLaser

Rh B dopedParticles

Mie Scattering

Fluorescence

LIFMIE

Temperature

If dye has T dependence…

Va Tech demonstration used first measurement approach described above(Lowe, VT)

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Phase I Results: Concept Demo II

• Split collected light into two channels: Mie (532 nm) & LIF (>600 nm)• Added dry ice to flow to vary temperature; monitor with thermocouple

June 5-7, 2012 NASA Aeronautics Mission Directorate FY11 Seedling Phase I Technical Seminar 21

5 Wlaser

PMT detection

(Lowe, VT)

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Phase I Results: Concept Demo III

• Mie scattering provided plenty of signal for velocimetry (though not demonstrated in this experiment).

• LIF channel provided sufficient signal for temperature determination (using Mie as reference)

• Temperature range in proposed experiments will be largerJune 5-7, 2012 NASA Aeronautics Mission Directorate FY11 Seedling Phase I Technical Seminar 22

No dye in PSL: With dye in PSL:

Mie

LIF

Mie

LIF

Scattering traces from single particles

(Lowe, VT)

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Distribution: Getting the Word Out

• Presentations:– Occurred: SERMACS-2011– Planned:

• ACS, MRS, or Equivalent for materials synthesis • AIAA meeting with PSL seeding characterization results

• Publications:– Demonstration work at VT is nearing

conference/journal publication quality results– PI’s have strong track record of publishing in

conferences and journals (see proposal appx)

June 5-7, 2012 NASA Aeronautics Mission Directorate FY11 Seedling Phase I Technical Seminar 23

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Proposed Budget

June 5-7, 2012 NASA Aeronautics Mission Directorate FY11 Seedling Phase I Technical Seminar 24

Proposal Title: Fluorescence-Doped Particles for Simultaneous Temperature and Velocity Imaging

From: 07/01/12To: 12/31/14

PI's Name: Paul DanehyNASA Center: LaRC

Assume $150K for 1 Full Time Equivalent of 2080 hours per NASA Civil Servant.Budget Request ($K) FY12 FY13 FY14 TOTAL

Civil Servant Salary: Paul Danehy PI (0.15 FTE) 6 22 6 34Civil Servant Salary: Patsy Tiemsin Co-I (0.3 FTE) 11 45 11 67Civil Servant Salary: Chris Wohl Co-I (0.2 FTE) 8 30 8 46Total Civil Servant Travel 3 3 6In-house Procurement - Materials 5 12 4 21External Procurement - Virginia Tech 15 58 15 88External Procurement - NIA (post-doc) 0 110 28 138

Budget Total 45 280 75 400

Cost Sharing, non-NASA Partner Provided Budget ($K) FY12 FY13 FY14 TOTALVirginia Tech 3 13.1 3 19.1

Total 3 13.1 3 19.1

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Future Plans I

• Continue to work with current/existing dyes– Rhodamine B: develop water seeder?– Fluorescein: try different variants

• Explore additional existing dyes– Literature search turned up good options to try– Additional literature search for existing dyes that

are not commercially available

• Continue to develop measurement instrumentation for T, P, LDV or PIV demonstrations: apply to supersonic free jet

June 5-7, 2012 NASA Aeronautics Mission Directorate FY11 Seedling Phase I Technical Seminar 25

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Future Plans II

• Amphiphilic, chemically reactive dye

June 5-7, 2012 NASA Aeronautics Mission Directorate FY11 Seedling Phase I Technical Seminar 26

Particle

Solvent

AmphiphilicDye

InterfacialRegion

• Design of a dye molecule to thermodynamically populate the interfacial region

• Functionalize the dye to chemically react with the styrene monomers

• Result:• Lower Loading• Reduced chance for

leaching• Greater sensitivity to

environmental temperature, pressure, etc.

(Grk: both love; water-loving and fat-loving properties; surfactant)

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Future Plans (Phase II Proposal)

June 5-7, 2012 NASA Aeronautics Mission Directorate FY11 Seedling Phase I Technical Seminar 27

0 3 6 9 12 15 18

Task

Months after Phase II Funding

Hire Postdoctoral Researcher

Synthesize Dye-Doped PSLs with COTS or Reported Dyes

Begin Amphiphilic Dye Synthesis

Synthesize Amphiphilic Dye-Doped PSLs

Finalize Dye-Doped PSL Synthesis

Dye/PSL Synthesis Activities

Demo / Test Activities

Velocity-Temperature LDV

Velocity-Pressure LDV

Velocity-Temperature PIV

(Jet expt)

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Conclusions• Developing new generation of particle-based

instrumentation for wind tunnels– Temperature, Pressure, Concentration measurements to

complement velocity and conventional instrumentation– Can use much of same equipment as LDV/PIV

• Have successfully doped Rh B dye into particles – Demonstrated temperature measurement at VT– Rh B is slightly toxic

• Can we find a way to safely use it?• Can we find other, safer options?

• Many options of other dyes to explore; may invent new dyes to meet requirements.

June 5-7, 2012 NASA Aeronautics Mission Directorate FY11 Seedling Phase I Technical Seminar 28

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June 5-7, 2012 NASA Aeronautics Mission Directorate FY11 Seedling Phase I Technical Seminar 29

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Phase I Results

Synthesis with MgSO4 Synthesis with ZnSO4

June 5-7, 2012 NASA Aeronautics Mission Directorate FY11 Seedling Phase I Technical Seminar 30

N

NN

NMg+2

N

NN

NZn+2

Green Color(expected) Burgundy Color

(expected)

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Phase I Results

Rhodamine-doped PSLsFluorescein & Kiton Red-doped PSL

June 5-7, 2012 NASA Aeronautics Mission Directorate FY11 Seedling Phase I Technical Seminar 31

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Fluorescent particle past work• Literature Review:• Found no past work using doped

PSL for thermometry• Kimura et al. (2006) used PSLs

painted with PSP to measure pressure.

• Fluorescein 27 is very attractive for temperature sensitivity, on the order of 3.5%/oC (Dunand et al. 2010 and Sutton et al. 2008)

• Multiple dye techniques may offer significant advantages for improved sensitivity (Sutton et al. 2008).

• US Patent 4194877 claims invention of dye-doped PSLs.

Pressure sensitive PSLs and results of Kimura et al. (2006).

Two-dye thermometry technique of Sutton et al. (2008).