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Displaying 1-50 of 74 results
Latent heat transfer : an introduction to fundamentals / G.S.H. Lock.
- Text
- Oxford, [England] ; New York : Oxford University Press, 1994.
- 1994
- 1 Item
Item details Format Call Number Item Location Text JSE 95-124 Offsite Nested subcritical flows within supercritical systems / R.C. Hendricks ... [and others].
- Text
- [Washington, D.C.] : National Aeronautics and Space Administration, [1985]
- 1985
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/LPS105611Experience with advanced instrumentation in a hot section cascade / Frederick C. Yeh and Herbert J. Gladden.
- Text
- [Washington, D.C.] : National Aeronautics and Space Administration, [1989]
- 1989
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/LPS108066The effects of inlet turbulence and rotor/stator interactions on the aerodynamics and heat transfer of a large-scale rotating turbine model : IV--aerodynamic data tabulation / R.P. Dring, H.D. Joslyn, and M.F. Blair.
- Text
- East Hartford, Conn. : United Technologies Research Center ; [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center, [1988]
- 1988
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/LPS112274Further shock tunnel studies of scramjet phenomena / R. G. Morgan ... [and others].
- Text
- [Washington, D.C.] : [National Aeronautics and Space Administration], [1986]
- 1986
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/LPS112727Investigation of the effects of pressure gradient, temperature, and wall temperature ratio on the stagnation point heat transfer for circular cylinders and gas turbine vanes [microform] / by H.T. Nagamatsu and R. E. Duffy.
- Text
- Troy, N.Y. : Rensselaer Polytechnic Institute, [1984]
- 1984
Analyses of physical-chemical processes governing SSME internal fluid flows [microform] : progress report for November 1984 / by A.K. Singhal ... [et al.] ; prepared for National Aeronautics and Space Administration, George C. Marshall Space Flight Center.
- Text
- [Huntsville, Ala.] : CHAM of North America, [1984]
- 1984
Burner liner thermal/structural load modeling [microform] / by R. Maffeo.
- Text
- Cincinnati, OH : General Electric Co., Aircraft Engine Business Group, [1984]
- 1984
Improvement of the second - and third-moment modeling of turbulence / by R. S. Amano and P. Goel.
- Text
- Milwaukee, Wis. : Dept. of Mechanical Engineering, University of Wisconsin ; Cleveland, Ohio : NASA Lewis Research Center, [1986]
- 1986
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo22001Gear mesh loss-of-lubrication experiments and analytical simulation / Robert F. Handschuh, Joseph Polly, and Wilfredo Morales.
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2011]
- 2011
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo24045Evaluation of capillary reinforced composites / by Samuel W. Ciardullo and Lewis J. Stoffer.
- Text
- Cincinnati, Ohio : General Electric Company, Aircraft Engine Business Group ; [Cleveland, Ohio] : National Aeronautics and Space Administration, NASA Lewis Research Center, [1985]
- 1985
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo24654Post-test analysis of a 10-year sodium heat pipe life test / John H. Rosenfeld ... [and others].
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2011]
- 2011
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo27051Design and test plans for a non-nuclear fission power system technology demonstration unit / Lee Mason ... [and others].
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2011]
- 2011
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo27080Flow boiling with enhancement devices for cold plate coolant channel design : final report / by Ronald D. Boyd, Sr.
- Text
- Prairie View, TX : Department of Mechanical Engineering, Prairie View A&M University ; [Houston, Tex.] : National Aeronautics and Space Administration (NASA) Lyndon B. Johnson Space Center, [1989]
- 1989
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo29929Effects of tip clearance and casing recess on heat transfer and stage efficiency in axial turbines / A.A. Ameri, E. Steinthorsson, David L. Rigby.
- Text
- [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center, [1998]
- 1998
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo30851Flow boiling with enhancement devices for cold plate coolant channel design [microform] : final report / by Ronald D. Boyd, Sr.
- Text
- Prairie View, TX : Department of Mechanical Engineering, Prairie View A&M University ; [Houston, Tex.] : National Aeronautics and Space Administration (NASA) Lyndon B. Johnson Space Center, [1989]
- 1989
Performance impact of deflagration to detonation transition enhancing obstacles / Daniel E. Paxson, Frederick Schauer and David Hopper.
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
- 2012
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo31854Investigation of surface tension driven convection as a feasibility study for a micro-gravity experiment : final report / E. L, Koschmieder.
- Text
- Cleveland, Ohio : NASA Lewis Research Center, [1988]
- 1988
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo31701A compendium of brazed microstructures for fission power systems applications / Ivan E. Locci, Cheryl L. Bowman.
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
- 2012
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo32072Investigation of surface tension driven convection as a feasibility study for a micro-gravity experiment [microform] : final report / E.L. Koschmieder.
- Text
- Cleveland, Ohio : NASA Lewis Research Center, [1988]
- 1988
The thermal-vortex equations : final report / John V. Shebalin.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1987]
- 1987
Thermosyphon flooding in reduced gravity environments test results / Marc A. Gibson [and three others].
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, July 2013.
- 2013-7
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo47646Influence of coolant tube curvature on film cooling effectiveness as detected by infrared imagery / S. Stephen Papell, Robert W. Graham, and Richard P. Cageao.
- Text
- Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, November 1979.
- 1979-11
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo52212Generalized Fluid System Simulation Program, version 6.0 / A.K. Majundar [and three others].
- Text
- Huntsville, Alabama : National Aeronautics and Space Administration, Marshall Space Flight Center, October 2013.
- 2013-10
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo53733Space station systems technology study, final report.
- Text
- [Huntsville, Ala.] : Boeing Aerospace Company, Spectra Research Systems : NASA Marshall Space Flight Center, February 1984.
- 1984-2
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo54001Parametric system model for a Stirling radioisotope generator / Paul C. Schmitz.
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, March 2015.
- 2015-3
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo59981Metallized gelled propellants : oxygen/RP-1/aluminum rocket heat transfer and combustion measurements / Bryan Palaszewski and James S. Zakany.
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, August 1996.
- 1996-8
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo70075RL10A-3-3A rocket engine modeling project / Michael Binder, Thomas Tomsik and Joseph P. Veres.
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, January 1997.
- 1997-1
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo70089Predicted turbine heat transfer for a range of test conditions / R.J. Boyle and B.L. Lucci.
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, November 1996.
- 1996-11
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo70711Wind-tunnel measurements and comparison with flight of the boundary layer and heat transfer on a hollow cylinder at Mach 3 / Robert L. Stallings, Jr., and Milton Lamb.
- Text
- [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, December 1980.
- 1980-12
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo71443Heat transfer computations of internal duct flows with combined hydraulic and thermal developing length / C.R. Wang [and three others].
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, May 1997.
- 1997-5
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo72606Development of a device to deploy fluid droplets in microgravity / David W. Robinson and An-Ti Chai.
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, July 1997.
- 1997-7
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo72614Overview of NASA multi-dimensional Stirling converter code development and validation effort / Roy C. Tew [and four others].
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, December 2002.
- 1992-12
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/LPS46696Approximation of engine casing temperature constraints for casing mounted electronics / Jonathan L. Kratz and Dennis E. Culley, Jeffryes W. Chapman.
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, April 2017.
- 2017-4
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo81330Modeling xenon tank pressurization using one-dimensional thermodynamic and heat transfer equations / Ryan P. Gilligan and Thomas M. Tomsik.
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, April 2017.
- 2017-4
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo81490Evaluation of heat transfer and thermal stability of supercritical JP-7 fuel / Diane L. Linne [and three others].
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, July 1997.
- 1997-7
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo79343A numerical method for incompressible flow with heat transfer / Jong-Youb Sa, Dochan Kwak.
- Text
- Moffett Field, California : National Aeronautics and Space Administration, Ames Research Center, April 1997.
- 1997-4
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo78588The effects of Reynolds number, rotor incidence angle and surface roughness on the heat transfer distribution in a large-scale turbine rotor passage / reported by M.F. Blair.
- Text
- East Hartford, Connecticut : United Technologies Research Center, November 1991.
- 1991-11
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/LPS62406Experimental and numerical characterization of a steady-state cylindrical blackbody cavity at 1100 degrees celsius / Thomas J. Horn, Amanie N. Abdelmessih.
- Text
- Edwards, California : National Aeronautics and Space Administration, Dryden Flight Research Center, August 2000.
- 2000-8
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/LPS31291Comparison of predicted and measured turbine vane rough surface heat transfer / R.J. Boyle, C.M. Spuckler, and B.L. Lucci.
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, December 2000.
- 2000-12
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo79758Infrared low temperature turbine vane rough surface heat transfer measurements / R.J. Boyle [and three others].
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, August 2000.
- 2000-8
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo79813Augmentation of stagnation region heat transfer due to turbulence from a DLN can combustor / G. James Van Fossen, Ronald S. Bunker.
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, July 2000.
- 2000-7
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/LPS30203Experimental heat transfer and bulk air temperature measurements for a multipass internal cooling model with ribs and bleed / Douglas Thurman, Philip Poinsatte.
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center : U.S. Army Research Laboratory, January 2000.
- 2000-1
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo85942Heat transfer measurements and computations on blade of variable speed power turbine blade cascade / Philip E. Poinsatte [and four others].
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, June 2020.
- 2020-6
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo150801Ten year operating test results and post-test analysis of a 1/10 segment stirling sodium heat pipe : phase III final report / John H. Rosenfeld, Kenneth G. Minnerly, and Christopher M. Dyson, Thermacore, Inc., Lancaster, Pennsylvania.
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, 2012.
- 2012
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo31113Quantitative global heat transfer in a Mach-6 quiet tunnel / John P. Sullivan [and ten others].
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2012]
- 2012
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo32903Computational work to support FAP/SRW variable-speed power-turbine development / Ali A. Ameri.
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
- 2012
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo32902Implementation of a transition model in a NASA code and validation using heat transfer data on a turbine blade / Ali A. Ameri.
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
- 2012
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo32880The thermal-vortex equations : final report / John V. Shebalin.
- Text
- Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, [1987]
- 1987
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo33838Two dimensional heat transfer around penetrations in multilayer insulation : final report / Wesley L. Johnson and Andrew O. Kelly, Kevin M. Jumper.
- Text
- Kennedy Space Center, FL : National Aeronautics and Space Administration, Kennedy Space Center, 2012.
- 2012
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo37064
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