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Duct flow nonuniformities for space shuttle main engine (SSME) [microform] : final report / by Lockheed Missiles & Space Company, Inc., Huntsville Engineering Center.
Text
Marshall Space Flight Center, AL : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1988]
1988
0 resources
Numerical simulation of the flow about the F-18 HARV at high angle of attack [microform] / Scott M. Murman.
Text
San Jose, CA : MCAT Institute ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
1994
0 resources
BladeCAD, an interactive geometric design tool for turbomachinery blades [microform] / Perry L. Miller ... [et al.].
Text
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
1996
0 resources
Three-dimensional Navier-Stokes analysis and redesign of an imbedded bellmouth nozzle in a turbine cascade inlet section [microform] / P.W. Giel ... [et al.].
Text
[Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
1996
0 resources
Flow boiling enhancement for thermal management systems [microform] : final report : from the Thermal Science Research Center (TSRC) / by Ronald D. Boyd [principal investigator].
Text
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1998]
1998
0 resources
Bubble generation in a continuous liquid flow under gravity conditions [microform] / Salvatore Cezar Pais.
Text
[Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Springfield, VA : National Technical Information Service, distributor, [1999]
1999
0 resources
Acoustic reflection and transmission of 2-dimensional rotors and stators, including mode and frequency scattering effects [microform] / Donald B. Hanson.
Text
[Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
1999
0 resources
Effect of jet injection angle and number of jets on mixing and emissions from a reacting crossflow at atmospheric pressure [microform] / D. St. John and G. S. Samuelsen.
Text
[Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Springfield, VA : National Technical Information Service, distributor, [2000]
2000
0 resources
Flows in pinned arrays simulating brush seals [microform] / R.C. Hendricks ... [et al.].
Text
[Cleveland, Ohio? : National Aeronautics and Space Administration, Lewis Research Center ; Springfield, Va. : For sale by the National Technical Information Service, 1996]
1996
1 resource
Available online
http://purl.access.gpo.gov/GPO/LPS60620An experimental comparison of nonswirling and swirling flow in a circular-to-rectangular transition duct [microform] / B. A. Reichert and W. R. Hingst, and T. H. Okiishi.
Text
[Cleveland, Ohio : Lewis Research Center, 1991]
1991
1 resource
Available online
http://purl.access.gpo.gov/GPO/LPS62060Analytical study of the origin and behavior of asymmetric vortices [microform] / Murray Tobak, David Degani, Gregory G. Zilliac.
Text
Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1990]
1990
1 resource
Available online
http://purl.access.gpo.gov/GPO/LPS67462A knowledge-based approach to automated flow-field zoning for computational fluid dynamics [microform] / Alison Andrews Vogel.
Text
Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1989]
1989
1 resource
Available online
http://purl.access.gpo.gov/GPO/LPS70935Reduction of the shock wave intensity by modifying the transsonic [i.e. transonic] blade trailing edge [microform] / Piotr Doerffer.
Text
Washington, D.C. : National Aeronautics and Space Administration, [1983]
1983
0 resources
BladeCAD : an interactive geometric design tool for turbomachinery blades / Perry L. Miller IV [and three others].
Text
Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, July 1996.
1996-7
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo69229Flows in pinned arrays simulating brush seals / R.C. Hendricks [and three others].
Text
Cleveland, Ohio : National National Aeronautics and Space Administration, Lewis Research Center, December 1996.
1996-12
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo70383Effects of forebody geometry on subsonic boundary-layer stability / S. S. Dodbele.
Text
[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1990.
1990
1 resource
Available online
https://purl.fdlp.gov/GPO/LPS60902No results found from Digital Research Books Beta
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