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Experimental study of vane heat transfer and aerodynamics at elevated levels of turbulence [microform] / Forrest E. Ames.
Text
[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1994.
1994
0 resources
High frequency flow/structural interaction in dense subsonic fluids [microform] / B.-L. Liu and J.M. O'Farrell.
Text
Marshall Space Flight Center, Ala. : National Aeronautics and Space Administration, Marshall Space Flight Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
NASA low-speed axial compressor for fundamental research [microform] / Charles A. Wasserbauer, Harold F. Weaver, Richard G. Senyitko.
Text
[Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1995.
1995
0 resources
Internal aerodynamics of a generic three-dimensional scramjet inlet at Mach 10 [microform] / Scott D. Holland.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Linthicum Heights, MD : NASA Center for AeroSpace Information, distributor ; Springfield, Va. : National Technical Information Service, distributor, [1995]
1995
0 resources
Advanced multi-phase flow CFD model development for solid rocket motor flowfield analysis [microform] : final report / by Paul Liaw and Yen-Sen Chen.
Text
Huntsville, AL : Engineering Sciences, Inc. ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
The acoustic characteristics of turbomachinery cavities [microform] / M.J. Lucas ... [et al.].
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[MSFC, Ala.] : National Aeronautics and Space Administration, Marshall Space Flight Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Contribution to the optimal shape design of two-dimensional internal flows with embedded shocks [microform] / Angelo Iollo, Manuel D. Salas.
Text
Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Comparison of numerical results and multicavity purge and rim seal data with extensions to dynamics [microform] / Mahesh M. Athavale ... [et al.].
Text
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
A root-mean-square pressure fluctuations model for internal flow applications [microform] / Y.S. Chen.
Text
[Washington, DC] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1985.
1985
0 resources
Final report on adaptive computational methods for SSME internal flow analysis [microform] / by J. Tinsley Oden.
Text
[Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1988]
1986
0 resources
NASA low-speed axial compressor for fundamental research [microform] / Charles A. Wasserbauer, Harold F. Weaver, Richard G. Senyitko.
Text
[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1995.
1995
0 resources
Laser doppler velocimeter system for subsonic jet mixer nozzle testing at the NASA Lewis Aeroacoustic Propulsion Lab [microform] / Gary G. Podboy ... [et al.].
Text
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Calculation of three-dimensional (3-D) internal flow by means of the velocity-vorticity formulation on a staggered grid [microform] / Paul M. Stremel.
Text
Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, VA : National Technical Information Service, distributor, 1995]
1995
0 resources
Computations of viscous flows in complex geometries using multiblock grid systems [microform] / Erlendur Steinthorsson and Ali A. Ameri.
Text
Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, Institute for Computational Mechanics in Propulsion ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Supersonic reacting internal flow fields [microform] / J. Philip Drummond.
Text
[Washington, D.C.? : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1990?]
1990
0 resources
3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet [microform] / M. Mizukami and J.D. Saunders.
Text
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Calculations of diffuser flows with an anisotropic K-[epsilon] model [microform] / J. Zhu and T.H. Shih.
Text
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Application of thin-film thermocouples to localized heat transfer measurements [microform] / J. Lepicovsky, R.J. Bruckner and F.A. Smith.
Text
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Heat transfer computations of internal flows with combined hydraulic and thermal developing length [microform] / C.R. Wang ... [et al.].
Text
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
1997
0 resources
SRM internal flow test and computational fluid dynamic analyses [microform] : final report : contract NAS8-39095 / prepared by ERC, Incorporated.
Text
Huntsville, AL : ERC, Inc. ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995- ]
1995-present
0 resources
A general fluid system simulation program to model secondary flows in turbomachinery [microform] / Alok K. Majumdar, Katherine P. Van Hooser.
Text
[Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Heat transfer experiments in the internal cooling passages of a cooled radial turbine rotor [microform] / B.V. Johnson and J.H. Wagner.
Text
[Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
1996
0 resources
Experimental study of vortex breakdown in a cylindrical, swirling flow [microform] / J.L. Stevens ... [et al.].
Text
[Stanford, Calif.] : Joint Institute for Aeronautics and Acoustics, National Aeronautics and Space Administration, Ames Research Center : Joint Institute for Aeronautics and Acoustics, Stanford University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
1996
0 resources
Variational methods in sensitivity analysis and optimization for aerodynamic applications [microform] : progress report for the period ended June 30, 1996 ... under research grant NCC1-68 / by A.H. Ibrahim, G.J.-W. Hou, and S.N. Tiwari, principal investigator ; submitted by the Old Dominion University Research Foundation.
Text
Norfolk , Va. : Dept. of Mechanical Engineering, College of Engineering & Technology, Old Dominion University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
1996
0 resources
Static investigation of a multiaxis thrust-vectoring nozzle with variable internal contouring ability [microform] / David J. Wing, Charles T.L. Mills, and Mary L. Mason.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
1997
0 resources
Laser anemometer measurements of the flow field in a 4:1 pressure ratio centrifugal impeller [microform] / G.J. Skoch ... [et al.].
Text
[Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
1997
0 resources
Ground based studies of thermocapillary flows in levitated drops [microform] : analytical part : final report (April 1, 1993 - December 31, 1996), NASA grant no.--NAGW-3378 / principal investigator, S.S. Sadhal; co-investigator, Eugene H. Trinh.
Text
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
1997
0 resources
Aerodynamic synthesis of a centrifugal impeller using CFD and measurements [microform] / L.M. Larosiliere and G.J. Skoch, P.S. Prahst.
Text
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
1997
0 resources
The kinetic nonequilibrium processes in the internal flow and in the plume of subsonic and supersonic aircrafts [microform] : summary of research, from August 28, 1996 to August 28, 1997, NAG3-1957 / Alexander M. Starik.
Text
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
1997
0 resources
PSP measurement of stator vane surface pressures in a high speed fan [microform] / Jan Lepicovsky.
Text
[Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
1998
0 resources
Euler flow computations on non-matching unstructured meshes [microform] / Udayan Gumaste.
Text
[Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Springfield, VA : National Technical Information Service, distributor, [1999]
1999
0 resources
Use of pressure sensitive paint for diagnostics in turbomachinery flows with shocks [microform] / Jan Lepicovsky, Timothy J. Bencic.
Text
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center ; Hanover MD : Available from NASA Center for AeroSpace Information, [2001]
2000
1 resource
Available online
Adobe Acrobat Reader requiredMach 10 experimental database of a three-dimensional scramjet inlet flow field [microform] / Scott D. Holland.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, VA : Available from the National Technical Information Service, 1995]
1995
1 resource
Available online
http://purl.access.gpo.gov/GPO/LPS60779Analysis of internal flow in a ventral nozzle for STOVL aircraft [microform] / C. Frederic Smith and Jack G. McArdle ; prepared for the 26th Joint Propulsion Conference cosponsored by the AIAA, SAE, ASME, and ASEE, Orlando, Florida, July 16-18, 1990.
Text
[Washington, D.C.] : NASA ; [Springfield, Va. : For sale by the National Technical Information Service, 1990]
1990
1 resource
Available online
http://purl.access.gpo.gov/GPO/LPS69189User's guide for NASCRIN--a vectorized code for calculating two-dimensional supersonic internal flow fields [microform] / Ajay Kumar.
Text
[Washington, D.C]. : National Aeronautics and Space Administration, Scientific and Technical Information Office, 1984.
1984
0 resources
Supersonic retropropulsion test 1853 in NASA LaRC Unitary Plan Wind Tunnel test section 2 / Scott A. Berry and Matthew N. Rhode.
Text
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, April 2014.
2014-4
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo54425Calculations of diffuser flows with an anisotropic K-[epsilon] model / . Zhu and T.-H. Shih.
Text
Cleveland, Ohio : National Aeronautics and Space AdministrationLewis Research Center, November 1995.
1995-11
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo67332Aerodynamic synthesis of a centrifugal impeller using CFD and measurements / L.M. Larosiliere and G.J. Skoch, P.S. Prahst.
Text
Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center : U.S. Army Research Laboratory, July 1997.
1997-7
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo73188A general fluid system simulation program to model secondary flows in turbomachinery / Alok K. Majumdar, Katherine P. Van Hooser.
Text
[Washington, D.C.] : National Aeronautics and Space Administration, [1996]
1996
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo79370A comparison of two incompressible Navier-Stokes algorithms for unsteady internal flow / N. Lyn Wiltberger, Stuart E. Rogers, and Dochan Kwak.
Text
Moffett Field, California : National Aeronautics and Space Administration, Ames Research Center, November 1993.
1993-11
1 resource
Available online
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