NASAIndustry
LPT Workshop August 2010 (Zip File)
Ameri, Ali A., Ajmani, Kumud, "Evaluation
of Predicted Heat Transfer on a Transonic Blade Using ν ^{2
}– ƒ Models", ASME Paper GT200453572, June
2004.
Ameri, A. A., Rigby, D. L., Steinthorsson, E., Gaugler, Raymond, "Computation
of Turbulent Heat Transfer on the Walls of a 180 Degree Turn Channel With a Low
Reynolds Number Reynolds Stress Model; Final Report", ASME paper
2002GT30211, April 2002, also NASA/CR200230211.
Ameri, Ali A., "Heat
Transfer and Flow on the Tip of a Gas Turbine Equipped with a MeanCamberline
Strip",
ASME paper 2001GT0156, June 2001, NASA/CR—2001210764.
Ameri, A. A. and Rigby, David L., "A
Numerical Analysis of Heat Transfer and Effectiveness on Film Cooled Turbine
Blade Tip Models", NASA/CR1999209165, July, 1999. Presented at 14th
ISABE, Florence,
Italy, September 510, 1999.
Ameri, A. A. and Bunker, R. S., "Heat
Transfer and Flow on the First Stage Blade Tip of a Power Generation Gas
Turbine, Part 2: Simulation Results", ASME paper 99GT283, June, 1999, , also NASA/CR1999209151, April,
1999.
Ameri, A. A., Steinthorsson, E. and Rigby, David L., "Effects of Tip Clearance and Casing Recess on Heat Transfer and
Stage Efficiency in Axial Turbines", ASME paper 98GT369, June, 1998, also NASA/CR1998208514, to be
published in ASME Journal of Turbomachinery.
Ameri, A. A., Steinthorsson, E. and Rigby, David L., "Effect of Squealer Tip on Rotor Heat Transfer and Efficiency", ASME paper 97GT128, June, 1997, & ASME Journal or Turbomachinery,
October, 1998, vol. 120, no. 4, pp. 753759.
Ameri, A. A. and Steinthorsson, E., "Analysis of Gas Turbine Rotor Blade Tip and Shroud Heat
Transfer", ASME paper 96GT189, June, 1996, also NASA CR 198541, Oct. 1996.
Ameri, A. A. and Steinthorsson, E., "Prediction of Unshrouded Rotor Blade Tip Heat Transfer", ASME paper 95GT142, June, 1995, also NASA CR 198542.
Ameri, A. A. and Arnone, A., "Transition Modeling Effects on Turbine Rotor Blade Heat Transfer
Predictions", ASME paper 94GT22, June, 1994, & ASME Journal of
Turbomachinery,
April, 1996, vol. 118, no. 2, pp. 307313.
Ameri, A. A. and Arnone, A., "Prediction of Turbine Blade Passage Heat Transfer Using a Zero and
a TwoEquation Turbulence Model", ASME paper 94GT122, June, 1994.
Ameri, A. A. and Arnone, A., "NavierStokes Turbine Heat Transfer Predictions Using TwoEquation
Turbulence Closures", AIAA paper 923067, July, 1992, also NASA TM 105817.
Ameri, A. A., Sockol, P. M. and Gorla, R. S. R., "NavierStokes Analysis of Turbomachinery Blade external Heat Transfer", Journal of Propulsion and Power Vol. 8. No., MarchApril 1992.
Ameri, A. A. and Arnone, A., "Three Dimensional
NavierStokes Analysis of Turbine Passage Heat
Transfer", AIAA paper 912241, June, 1991.
Ashpis, David E.," Dust Removal From Solar Cells", United States
Patent US 7,999,173 B1, August 16, 2011.
Ashpis, David E. and Thurman, Douglas R.,
"DBD
Plasma Actuators for Flow Control in Air Vehicles and Jet Engines  Simulation
of Flight Conditions in Test Chambers by Density Matching", NASA/TM 
2011217006, July 2011.
Ashpis, David E. and Thurman, Douglas R., "Test
Conditions for Performance Characterization of Dielectric Barrier Discharge
(DBD) Plasma Actuators for Active Flow Control in Jet Engines", ASME
paper GT201146583, June 2011.
Azad, Gm S., Han, JeChin and Boyle, Robert J., "Heat Transfer and
Flow on Squealer Tip of a Gas Turbine Blade", ASME paper 2000GT0195,
May 2000.
Azad, Gm S., Han, JeChin, Teng, Shuye and Boyle, Robert J., "Heat
Transfer and Pressure Distributions on a Gas Turbine Blade Tip", ASME
paper 2000GT0194, May 2000.
Boyle, Robert J., "Effects of
Thermal Barrier Coatings on Approaches to Turbine Blade Cooling", ASME
paper GT200691202, May 2006.
Boyle, Robert J., Senyitko, Richard G., "Effects of Surface Roughness on
Turbine Vane Heat Transfer", ASME paper GT200569133, June 2005.
Boyle, Robert J., Giel, P. W., and Ames, Forrest E., "Predictions
for the Effects of Freestream Turbulence on Turbine Blade Heat Transfer",
ASME paper GT200454332, NASA/TM2004213079, May 2004.
Boyle, Robert J., Senyitko, Richard G., "Measurements and Predictions of
Surface Roughness Effects on Turbine Vane Aerodynamics", ASME paper
GT200338580.
Boyle, Robert J., Lucci, Barbara L., Senyitko, Richard G., "Aerodynamic
Performance and Turbulence Measurements in a Turbine Vane Cascade",
ASME paper 2002GT30434, May 2002, also NASA/TM2002211709, November 2002.
Boyle, Robert J. and Giel, P.W., "Effect
of Favorable Pressure Gradients on Turbine Blade Pressure Surface Heat
Transfer", NASA/CP2001210888, April 2002.
Boyle, Robert J. and Giel, Paul W., "Prediction of Relaminarization
Effects on Turbine Blade Heat Transfer", ASME paper 2001GT0162, June
2001.
Boyle , Robert J., Lucci, B.L. and Spuckler, C.M., "Comparison of
Predicted and Measured Turbine Vane Rough Surface Heat Transfer", ASME
paper 2000GT0217, May 2000.
Boyle, Robert J., Lucci, B.L., Spuckler, C.M. and Camperchioli, W.P., "Infrared
Low Temperature Turbine Vane Rough Surface Heat Transfer Measurements",
ASME paper 2000GT0216, May 2000.
Boyle, R. J. and Simon, F. F., "Mach
Number Effects on Turbine Blade Transition Length
Prediction", ASME paper 98GT367, June 1998, also NASA/TM1998208404.
Boyle, R. J., Lucci, B. L., Verhoff, V. G., Camperchioli, W. P. and La,
H., "Aerodynamics of a Transitioning Stator over a Range of
Reynold's Numbers", ASME paper 98GT285, June 1998, also NASA/TM1998208408.
Boyle, R. J. and Giel, P. W., "Prediction of Nonuniform Inlet Temperature Effects on Vane and
Rotor Heat Transfer", ASME paper 97GT133, June 1997.
Boyle, R. J. and Lucci, B. L., "Predicted Turbine Heat Transfer for a Range of Test
Conditions", ASME paper 96GT304, June 1996, also NASA TM 107374, Nov. 1996.
Boyle, R. J. and Jackson, R., "Heat Transfer Predictions for Two Turbine Nozzle Geometries at High
Reynolds and Mach Number", ASME Paper 95GT104, June, 1995, & ASME Journal of
Turbomachinery,
vol. 119, no. 2, pp. 270283, April, 1997.
Boyle, R. J. and Ameri, A. A., "Grid Orthogonality Effects on Predicted Turbine Midspan Heat
Transfer and Performance", ASME Paper 94GT123, June, 1994.
Boyle, R. J., "Prediction of
Incidence and Surface Roughness Effects on Turbine
Performance", ASME Paper 93GT280, May 1993.
Boyle, R. J. and Giel, P. W., "ThreeDimensional
NavierStokes Heat Transfer Predictions for
Turbine Blade Rows", AIAA paper 923068, July, 1992, also NASA TM105800,July 1992, & AIAA
Journal of Prop. and Power, Vol. 11, No. 6, pp. 11791186, 1995.
Boyle, R. J. and Civinskas, K. C., "TwoDimensional
NavierStokes Heat Transfer Analysis", NASATM106008.
Boyle, R. J., "NavierStokes Analysis of Turbine Blade Heat Transfer", ASME Journal of
Turbomachinery, July 1991 Vol. 113 pp. 392403.
Boyle, R. J. and Russell, L. M., "Experimental Determination of Stator Endwall Heat Transfer", ASME Paper 89GT219, and ASME J. of
Turbomachinery, July 1990 Vol. 112
pp. 547558.
Bunker, R. S., Bailey, J. C. and Ameri, A. A., "Heat Transfer and Flow on the First Stage Blade Tip of a Power
Generation Gas Turbine, Part 1: Experimental Results", ASME paper 99GT169, June, 1999, also NASA/CR1999209152, April, 1999.
Camci, C., Kim, K., Hippensteele, S. A. and Poinsatte, P. E., "Convection Heat Transfer at the Curved Bottom Surface of a Square
to Rectangular Transition Duct Using a New Hue Capturing Based Liquid
Crystal Technique", ASME Fundamental Experimental Measurements in Heat TransferHTD Vol. 179,
pp. 722, 1991 and ASME Journal of Heat Transfer (in color), Vol. 115, pp.
311324.
Camci, C., Kim, K. and Hippensteele, S. A., "A New Hue Capturing Technique for the Quantitative Interpretation
of Liquid Crystal Images Used in Convective Heat Transfer Studies", ASME Paper 91GT122 and ASME Journal of
Turbomachinery, Vol. 114, pp.
765775, 1992.
Chen, J., Webster, R., Skoch, G. J., Herrick, G. P., Hathaway, M. D., "Technology
for Stabalizing the Compression System of a US Army Helicopter Gas Turbine
Engine: Validation of Unsteady Simulations", American Helicopter
Society, 61st Annual Forum & Technology Display, "New Frontiers in
Vertical Flight," Grapevine, TX, June 13, 2004.
Chen, S.C., Veres, J. P., Fitje, J. E., "Turbopump
Design and Analysis Approach for Nuclear Thermal Rocket", 2005.
Chima, R. V. and Liou, M.S., "Comparison
of the AUSM+ and HCusp Schemes for Turbomachinery Applications", AIAA
Paper AIAA20034120, June 2003, also NASA TM2003212457.
Chima, R. V., "Calculation of Multistage
Turbomachinery Using Steady Characteristic Boundary Conditions", AIAA
Paper 980968, Jan. 1998, also NASA TM1998206613.
Chima, R. V., Giel, P. W. and Boyle, R. J., "An Algebraic Turbulence Model for ThreeDimensional Viscous
Flows", NASA TM105931, presented at the 31st AIAA Aerospace Sciences Meeting,
Reno, Nevada, January 1114, 1993.
Chima, R. V., "Viscous ThreeDimensional
Calculations of Transonic Fan Performance", in CFD Techniques for
Propulsion Applications, AGARD Conference Proceedings No. CP510, AGARD,
NeuillySurSeine, France, Feb. 1992, pp 211 to 2119, also NASA TM103800.
Civinskas, K. C., Boyle, R. J. and McConnaughey, H. V., "Turbine Blading Designed for High Heat Load Space Propulsion
Applications", AIAA J. of Propulsion and Power, Sept.Oct. 1990 Vol. 6 pp. 598611.
Cully, D., Bright, M. M., Prahst, P. S. and Strazisar, A. J., "Active
Flow Separation Control of a Stator Vane Using Surface Injection in a Multistage
Compressor Experiment", ASME Paper GT200338863, June, 2003, also NASA
TM2003212356.
Dorney, D. J., Ashpis, David E., Halstead, David E. and Wisler, David C., "Study
of Boundary Layer Development in a TwoStage Low Pressure", AIAAJournal of Propulsion and Power, vol 16, no 1, pp160163, February, 2000.
Dorney, Daniel J., Flitan, Horia C., Ashpis, David E. and Solomon, William
J., "The Effects of Blade Count on Boundary Layer Development in a Low
Pressure Turbine", AIAA20000742, January, 2000, also
NASA/TM2000209911, Jan. 2000.
Dorney, Daniel J., Lake, James P., King, Paul I. and Ashpis, David E., "Experimental
and Numerical Investigation of Losses in Low Pressure Turbine Blade Rows",
AIAA20000737, January, 2000, also NASA/TM2000209910, Jan. 2000.
Dorney, D. J. and Ashpis, David E., "Study of Low Reynolds Number
Effects on the Losses in Low Pressure Turbine Blade rows",
International Journal of Turbo and Jet Engines, vol 16, pp91105, December,
1999.
Dorney, D. J., Ashpis, David E., Halstead, David E. and Wisler, David C., "Study of Boundary Layer Development in a TwoStage Low
Pressure", AIAA990742, January, 1999, also NASA/TM1999208913, Feb. 1999.
Dorney, D. J. and Ashpis, David E., "Study of Low Reynolds Number Effects on the Losses in Low Pressure
Turbine Blade rows", AIAA983575, July, 1998, also NASA/TM1998207919.
Dorney, D. J. and Schwab, J. R., "Unsteady Numerical Simulations of Radial Temperature Profile
Redistribution in a SingleStage Turbine", ASME Paper 95GT178, June, 1995.
Dunn, M. G., Kim, J., Civinskas, K. C. and Boyle, R. J., "TimeAveraged Heat Transfer and Pressure Measurements and
Comparison with Predictions for a TwoStage Turbine", ASME Paper 92GT194 and ASME J. of
Turbomachinery, Jan. 1994 Vol. 116
pp. 1423.
Garg, Vijay K., "LowPressure Turbine
Separation Control: Comparison With Experimental Data",
NASA/CR2002211689.
Garg, Vijay K. and Ameri, Ali A., "TwoEquation Turbulence Models for
Prediction of Heat Transfer on a Transonic Turbine Blade", ASME paper
2001GT0165, June 2001, NASA/CR2001210810.
Garg, V. K., "Heat
Transfer in Gas Turbines", NASA CR2001210942, March, 2001.
Presented at Turbulent Heat Transfer III, Girdwood, Alaska.
Garg, V. K., "Modeling FilmCoolant Flow Characteristics at the Exit
of ShowerHead Holes", ASME Paper , NASA/CR2000210510, October, 2000.
Garg, V. K., "Heat Transfer on a FilmCooled Rotating Blade Using Different
Turbulence Models", International Journal of Heat and Mass Transfer 42 (1999), pp. 789802.
Garg, V. K., "Heat
Transfer on a FilmCooled Rotating Blade", ASME Paper 99GT044, June,
1999, also NASA/CR1999209301, July, 1999.
Garg, V. K. and Rigby, D. L., "Heat transfer on a Film Cooled Blade  Effect of Hole Physics",
Int. J. of Heat & Fluid Flow 20 (1999) 1025.
Garg, V. K., "Heat Transfer on a FilmCooled Rotating Blade Using a TwoEquation
Turbulence Model", International Journal of Rotating Machinery, 1998, Vol. 4, No. 3, pp.
201216.
Garg, V. K. and Rigby, D. L., "Heat
transfer on a Film Cooled Blade  Effect of Hole Physics", ASME Paper
98GT404, June, 1998, also NASA/CR1998206609. Accepted for publication in
Int. J. of Heat & Fluid Flow.
Garg, V. K., "Heat
Transfer in Film Cooled Turbine Blades", Proceedings 3rd ISHMTASME
Heat and Mass Transfer Conference, December, 1997.
Garg, V. K., "Adiabatic Effectiveness and Heat Transfer Coefficient on a
FilmCooled Rotating Blade", In Numerical Heat Transfer, Part A, 32:811830, 1997.
Garg, V. K. and Abhari, R. S., "Comparison of Predicted and Experimental Nusselt Number for a
FilmCooled Rotating Blade", International Journal of Heat and Fluid Flow, Vol. 18, No. 5, pp.
452460, 1997.
Garg, V. K. and Ameri, A. A., "Comparison
of TwoEquation Turbulence Models for Prediction of Heat Transfer on FilmCooled
Turbine Blades", In Numerical Heat Transfer, Part A, 31:347371, 1997.
Garg, V. K. and Ameri, A. A., "Comparison
of TwoEquation Turbulence Models for Prediction of Heat Transfer on FilmCooled
Turbine Blades", ASME Paper 97GT024, June, 1997.
Garg, V. K., "Comparison of Predicted and Experimental Heat Transfer on a
FilmCooled Rotating Blade Using a TwoEquation Turbulence Model", ASME Paper 97GT220, June, 1997.
Garg, V. K. and Abhari, R. S., "Comparison of Predicted and Experimental Nusselt Number for a
FilmCooled Rotating Blade", ASME Paper 96GT223, June, 1996.
Garg, V. K., "Adiabatic Effectiveness and Heat Transfer Coefficient on a
FilmCooled Rotating Blade", ASME Paper 96GT221, June, 1996.
Garg, V. K. and Gaugler, R. E., "Leading
Edge Film Cooling Effects on Turbine Blade Heat Transfer", In Numerical
Heat Transfer, Part A, 30:165187, 1996.
Garg, V. K., "Effect of Blade Rotation on Film Cooling of Turbine
Blades", Proceedings 2nd ISHMTASME Heat and Mass Transfer Conference, pp 595600,
December, 1995.
Garg, V. K. and Gaugler, R. E., "Effect of Coolant Temperature and Mass Flow on Film Cooling of
Turbine Blades", ASME Paper 95WA/HT1, Nov., 1995; also in International Journal of Heat
and Mass Transfer, Vol. 40, No. 2, pp. 435445, 1997.
Garg, V. K. and Gaugler, R. E., "Leading
Edge Film Cooling Effects on Turbine Blade Heat Transfer", ASME Paper
95GT275, June, 1995, also NASA TM 106955, June, 1995.
Garg, V. K. and Gaugler, R. E., "Effect
of Velocity and Temperature Distribution at the Hole Exit on Film Cooling of
Turbine Blades", ASME Paper 95GT2, June, 1995, & ASME Journal of
Turbomachinery, Vol. 119, No. 2, pp. 343351, April 1997.
Garg, V. K. and Gaugler, R. E., "Prediction
of Film Cooling on Gas Turbine Airfoils", ASME Paper 94GT16, June,
1994; also NASA TM10653.
Garg, V. K. and Gaugler, R. E., "Heat Transfer in Film Cooled Turbine
Blades", ASME Paper 93GT81, May, 1993.
Garg, V. K., "Film Cooled Turbine Vane Heat Transfer", In Proceedings of the IMACSInternational Symposium on Scientific
Computing and Mathematical Modeling, December, 1992.
Giel, Paul W., Boyle, Robert J., Bunker, Ronald S., "Measurements and
Predictions of Heat Transfer on Rotor Blades in a Transonic Turbine
Cascade", ASME Paper GT200338839, June 2003, ASME J. of Turbomachinery, Vol 126, No.
1, pp.110121, January 2004
Giel, Paul W., Bunker, Ronald S. , Van Fossen, G. James and Boyle, Robert J.,
" Heat Transfer Measurements and Predictions on a Power Generation Gas
Turbine Blade", ASME paper 2000GT0209, May 2000.
Giel P. W., VanFossen, G. J., Boyle, R. J., Thurman, D. R, and Civinskas,
K. C., "Blade
Heat Transfer Measurements and Predictions in a Transonic Turbine Cascade",
ASME 99GT125, June, 1999, also NASA/TM1999209296.
Giel P. W., Thurman, D. R., Lopez, I., Boyle, R. J. and VanFossen, G. J.,
Jett, T. A., Camperchioli, W. P. and La, H., "ThreeDimensional
Flow Field Measurements in a Transonic Turbine Cascade", ASME
96GT113, June, 1996, accepted for publication in the ASME J. of Turbomachinery.
Giel P. W., Thurman, D. R., VanFossen, G. J., Hippensteele, S. A. and
Boyle, R. J., "Endwall
Heat Transfer Measurements in a Transonic Turbine Cascade", ASME
96GT180, June, 1996, recommended for publication in the ASME J. of
Turbomachinery.
Giel P. W., Sirbaugh, J. R., Lopez, I. and Van Fossen, G. J., "ThreeDimensional
NavierStokes Analysis and Redesign of an Imbedded Bellmouth Nozzle in a Turbine
Cascade Inlet Section", ASME Paper No. 94GT237, June, 1994, &
ASME Journal of Turbomachinery, Vol. 118, pp. 529535, July 1996.
Giel, P. W. and Schmidt, F. W., "A Comparison of Turbulence Modeling Predictions to Experimental
Measurements for High Rayleigh Number Natural Convection In Enclosures",
Proc. Ninth International Heat Transfer Conference, Jerusalem, Israel,
Vol. 2, pp. 175180, 1990.
Goldman, L. J., "ThreeDimensional Laser Anemometry in Annular Cascades",
in Advanced Methods for Cascade Testing, AGARDograph 328, pp. 170185,
August, 1993.
Goldman, L. J., "Laser
Anemometer Measurements and Computations for Transonic Flow Conditions in an
Annular Cascade of High Turning Core Turbine Vanes", NASA TP3383,
July, 1993.
Goldman, L. J. and Seasholtz, R. G., "Laser Anemometer Measurements and Computations in an Annular
Cascade of High Turning Core Turbine Vanes", NASA TP3252, July, 1992.
Goldman, L. J., "ThreeComponent Laser Anemometer Measurement Systems",
NASA TP3080, January, 1991.
Hah, C., Bergner, J. and Schiffer, H.P., "Short
LengthScale Rotating Stall Inception in a Transonic Axial Compressor  Criteria
and Mechanisms", ASME Paper GT200690045, May, 2006.
Hah, C., Rabe, D. C. and Wadia, A. R., "Role
of Tip Leakage Vortices and Paddage Shock in a Swept Transonic Compressor
Rotor", ASME Paper GT200453867, June, 2004.
Hathaway, M. D., Chen, J. and Webster, R., "Time
Accurate Unsteady Simulations of the Stall Inception Process in the Compression
System of a U.S. Army Helicopter Gas Turbine Engine", 2004 DOD High
Performance Computing Modernization Program User's Group Conference, Bellevue,
WA, June 710, 2004.
Hathaway, M. D., Chen, J. and Webster, R., "Time
Accurate Unsteady Simulations of the Stall Inception Process in the Compression
System of a U.S. Army Helicopter Gas Turbine Engine", 2003 DOD High
Performance Computing Modernization Program User's Group Conference, Bellevue,
WA, June 913, 2003.
Hathaway, M. D., "Self Recirculating
Casing Treatment Concept for Enhanced Compressor Performance", ASME
Paper GT200230368, July, 2002, also NASA TM2002211569 or ARLTR2748.
Heidmann, James D., Ameri, Ali A., Garg, Vijay K., Rigby, David L., "Improved
Modeling Capabilities in GlennHT  The NASA Glenn Research Center General
MultiBlock NavierStokes Heat Transfer Code", presented at the JANNAF
27th Airbreathing Propulsion Subcommittee Meeting, Colorado Springs, CO,
December 2003.
Heidmann, James D., Kasab, Alain J., Divo, Eduardo A., Rodriguez, Franklin,
Steinthorsson, Erlendur, "Conjugate
Heat Transfer Effects on a Realistic FilmCooled Turbine Blade", ASME
Paper GT200338553, June 2003.
Heidmann, James D. and Hunter, Scott D., "Coarse Grid Modeling of
Turbine Film Cooling Flows Using Volumetric Source Terms", ASME paper
2001GT0138, June 2001.
Heidmann, James D., Rigby, David L. and Ameri, Ali A., "A
ThreeDimensional Coupled
Internal/External Simulation of a FilmCooled Turbine
Vane", ASME Paper 99GT186, June, 1999, also NASA/CR1999209078,
April, 1999.
Heidmann, James D., Lucci, Barbara L. and Reshotko, Eli, "An
Experimental Study of the Effect of Wake Passing on Turbine Blade Film
Cooling", ASME Paper 97GT255, June, 1997.
Heidmann, James D., "The Effect of Wake Passing on Turbine Blade Film Cooling",
NASA TM107380, Ph.D. Thesis, Case western reserve University, January,
1997.
Heidmann, James D., "A
Numerical Study of the Effect of Wake Passing on Turbine Blade Film
Cooling", AIAA Paper 953044, July 1995.
Heidmann, James D., "Determination of a Transient Heat Transfer Property of Acrylic
Using Thermochromic Liquid Crystals", NASA TM106541, & AIAA Paper 940124, January, 1994.
Heidmann, James D., "A ThreeDimensional
NavierStokes Stage Analysis of the Flow
Through a Compact Radial Turbine", NASA TM104420, & AIAA Paper 912564, June, 1991.
Heidmann, James D., "An Analysis of the Viscous Flow Through a Compact Radial Turbine by
the Average Passage Approach", NASA TM102471, & ASME 90GT64, June, 1990.
Hippensteele, Steven A., "1996
Coolant Flow Management Workshop", NASACP10195, 1997.
Hippensteele, Steven A., "FilmCooling
HeatTransfer Measurements Using Liquid Crystals", 1997.
Hippensteele, S. A. and Poinsatte, P. E., "Transient
LiquidCrystal Technique Used to Produce HighResolution Convective
HeatTransferCoefficient Maps", Visualization of Heat Transfer
ProcessesHTD Vol. xx, pp. xx; and NASA TM 106083, 1993.
Larosiliere, L. M., Wood, J. R. and Hathaway M. D., "Aerodynamic Design Study of Advanced Multistage Axial
Compressor", NASA TP2002211568, Dec., 2002, also ARLTR2859.
Lau, S. C., Russell, L. M., Thurman, D. R. and Hippensteele, S. A., "Visualization of Local Heat Transfer in Pin Fin Channels with
Liquid Crystals", Fifth International Symposium on Transport Phenomena and Dynamics of
Rotating Machinery in Maui, Hawaii, May 811, 1994; and Journal of Flow
Visualization and Image Processing, Vol. 2.
Lau, S. C., Russell, L. M., Thurman, D. R. and Hippensteele, S. A., "Visualization of Local Heat Transfer in a Serpentine Channel with
Liquid Crystals", Fifth International Symposium on Transport Phenomena and Dynamics of
Rotating Machinery in Maui, Hawaii, May 811, 1994.
Lepicovsky, J., Braunscheidel, E. P., Bruckner, R. J., and Tweedt, D. L., "Laser Velocimeter Measurements of Axial Velocity Field in the NASA Supersonic Fan Rotor," ASME Paper 20001GT0333, June, 2001.
Lewalle, Jacques, Ashpis, David E. and Sohn, KiHyeon, "Demonstration
of Wavelet Techniques in the Spectral Analysis of Bypass Transition Data",
NASA TP3555, December, 1997.
Lewalle, Jacques and Ashpis, David E., "Transport in Bypass Transition: Mapping Active Time Scales using
Wavelet Techniques", Tenth Symposium on Turbulent Shear Flows, The Pennsylvania State
University, Vol. 2, pp. P237 – P242, August, 1995.
Lin, Y.L., Shih, T. I. P., Civinskas, K. C., Rigby, D. L. and Ameri, A.
A., "Nonlinear Versus Linear kw Model for
Predicting Flow and Heat transfer in a Smooth UDuct", AIAA paper AIAA983560, July, 1998.
Merchant, A., Kerrebrock, J. L., Adamczyk. J. J., and Braunscheidel, E., "Experimental Investigation of a High Pressure Ratio Aspirated Fan Stage," ASME Paper GT200453679, Sept, 2004. Also NASA TM2004213080.
Ng, Daniel and Spuckler, Charles M., "Application
of the Self Calibrating Emissivity and/or Transmissivity Independent
Multiwavelength Pyrometer to Measure the temperatures of Tungsten and Refractory
Material Surfaces", NASA TM 107152, January, 1996.
Ng, Daniel and Spuckler, Charles M., "A
NonContact Thermal Barrier Coating (TBC) Heat Flux Sensor Using a Self
Calibrating Multiwavelength Pyrometer", NASA TM 107150, January, 1996.
Ng, Daniel and Spuckler, Charles M., "NonContact
Heat Flux Measurement Using a Transparent Sensor", NASA TM 106252,
July, 1993.
Rigby, David L. and Bunker, Ronald S., "Heat
Transfer in a Complex Trailing Edge Passage for a High Pressure Turbine
Blade", NASA/CR2002211701, 2002.
Rigby, David L. and Lepicovsky, Jan, "Conjugate Heat Transfer
Analysis of Internally Cooled Configurations", ASME paper 2001GT0405,
June 2001.
Rigby, David L., "Numerical Simulation
of NonRotating and Rotating Coolant Channel Flow Fields", 2000.
Rigby, David L., "Prediction
of Heat and Mass Transfer in a Rotating Ribbed Coolant Passage with a 180 Degree
Turn", ASME Paper 98GT329, June, 1998, also NASA/TM1999208501.
Rigby, David L., Steinthorsson, E. and Ameri, A. A., "Numerical Prediction of Heat Transfer in a Channel with Ribs and
Bleed", ASME Paper 97GT431, June, 1997.
Rigby, David L., Steinthorsson, E. and Coirier, William J., "Automatic Block Merging Using the Method of Weakest Descent",
AIAA Paper 970197, January, 1997.
Rigby, David L., Ameri, Ali A. and Steinthorsson, Erlendur, "On
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