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The effects of vortex ingestion on the flow in a diffusing S-DUCT [microform] / B.J. Wendt and B.A. Reichert.
Text
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
1994
0 resources
An aerodynamic analysis of a mixed flow turbine [microform] / Chan M. Kim and Kestutis C. Civinskas.
Text
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
1994
0 resources
Numerical solution of the incompressible Navier-Stokes equations [microform] / Stuart E. Rogers.
Text
Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1990]
1990
0 resources
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
Dual active surface heat flux gage probe [microform] / Curt H. Liebert and Paul Kolodziej.
Text
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Recent improvements to and validation of the one dimensional NASA wave rotor model [microform] / Daniel E. Paxson and Jack Wilson.
Text
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Study of compressible flow through a rectangular-to-semiannular transition duct / Jeffry Foster ... [et al.].
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
Thermodynamic evaluation of transonic compressor rotors using the finite volume approach [microform] : status report, August 1986 on NASA grant no. NAG 3-593 / by Stephen Nicholson, John Moore.
Text
Blacksburg, Va. : Mechanical Engineering Dept., Virginia Polytechnic Institute and State University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1986]
1986
0 resources
Solution of the three-dimensional Helmholtz equation with nonlocal boundary conditions [microform] / Steve Hodge, William E. Zorumski, and Willie R. Watson.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [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
Mixing of multiple jets with a confined subsonic crossflow [microform]. Part II, opposed rows of orifices in rectangular ducts / James D. Holdeman, David S. Liscinsky, Daniel B. Bain.
Text
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
1997
0 resources
Flow through a rectangular-to-semiannular diffusing transition duct [microform] / Jeff Foster ... [et al.].
Text
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
1997
0 resources
The effects of acoustic treatment on pressure disturbances from a supersonic jet in a circular duct [microform] / Milo D. Dahl.
Text
[Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
1996
0 resources
Time-dependent parabolic finite difference formulation for harmonic sound propagation in a two-dimensional duct with flow [microform] / Kenneth J. Baumeister and Kevin L. Kreider.
Text
[Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
1996
0 resources
Wave rotor demonstrator engine assessment [microform] / Philip H. Snyder.
Text
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
1996
0 resources
Quick-mixing studies under reacting conditions [microform] : under grant NAG3-1110 / May Y. Leong and G.S. Samuelsen.
Text
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
1996
0 resources
Experimental and theoretical study of flow fields around ducted-nacelle models [microform] / Robert J. Mack.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
1998
0 resources
Perfectly matched layer for linearized Euler equations in open and ducted domains [microform] / C.K.W. Tam and L. Auriault, F. Cambuli.
Text
Reston, Va. : American Institute of Aeronautics and Astronautics ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1998]
1998
0 resources
An 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/LPS62060Analysis 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/LPS69189Thermodynamic evaluation of transonic compressor rotors using the finite volume approach for the period 12/20/84 - 12/19/85 [microform] : annual report on NASA grant no. NAG 3-593 / by John Moore, Stephen Nicholson, Joan G. Moore.
Text
Blacksburg, Va. : Mechanical Engineering Dept., Virginia Polytechnic Institute and State University ; Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, [1985]
1985
0 resources
A survey of oscillating flow in Stirling engine heat exchangers [electronic resource] / Terrence W. Simon and Jorge R. Seume.
Text
[Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center, [1988]
1988
1 resource
Available online
http://purl.access.gpo.gov/GPO/LPS113692A survey of oscillating flow in Stirling engine heat exchangers [microform] / Terrence W. Simon and Jorge R. Seume.
Text
[Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center, [1988]
1988
1 resource
Available online
http://purl.access.gpo.gov/GPO/LPS113692Mean veoIocity and turbulence measurements in a 90⁰ curved duct with thin inlet boundary layer [microform] : final report / R. A. Crawford ... [et al.].
Text
Tullahoma, Tenn. : University of Tennessee Space Institute, [1985]
1985
0 resources
Mean velocity and turbulence measurements in a 90° curved duct with thin inlet boundary layer : final report / R. A. Crawford ... [and others].
Text
Tullahoma, Tenn. : University of Tennessee Space Institute ; [Cleveland, Ohio] : NASA Lewis Research Center, [1985]
1985
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo22000The effects of acoustic treatment on pressure disturbances from a supersonic jet in a circular duct / Milo D. Dahl.
Text
Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, November 1996.
1996-11
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo70672Time-dependent parabolic finite difference formulation for harmonic sound propagation in a two-dimensional duct with flow / Kenneth J. Baumeister and Kevin L. Kreider.
Text
Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, November 1996.
1996-11
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo70683Heat 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/gpo72606Experimental and theoretical study of flow fields around ducted-nacelle models / Robert J. Mack.
Text
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, May 1998.
1998-5
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo83035No results found from Digital Research Books Beta
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