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Theory of finite disturbances in a centrifuglal compression system with a vaneless radial diffuser [microform] / F.K. Moore.
Text
[Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1990]
1990
0 resources
The effect of prewhirl on the internal aerodynamics nad performance of a mixed flow research centrifugal compressor [microform] / William B. Bryan and Sanford Fleeter.
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West Lafayette, Ind. : Thermal Sciences and Propulsion Center, School of Mechanical Engineering, Purdue University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1987]
1987
0 resources
Laser anemometer measurements of the three-dimensional rotor flow field in the NASA low-speed centrifugal compressor [microform] / Michael D. Hathaway ... [et al.].
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
Unsteady flow field in a multistage axial flow compressor [microform] / N. Suryavamshi, B. Lakshminarayana, J. Prato.
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University Park, PA : Center for Gas Turbine and Power, The Pennsylvania State University ; [Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center ; Springfield, Va. : National Technical Information Service, distributor, 1997]
1997
0 resources
Coordinates for a high performance 4:1 pressure ratio centrifugal compressor [microform] / Ted F. McKain and Greg J. Holbrook.
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[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
1997
0 resources
Forced response testing of an axi-centrifugal turboshaft engine [microform] / A. Karl Owen ... [et al.].
Text
[Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
1996
0 resources
Dynamic modeling of starting aerodynamics and stage matching in an axi-centrifugal compressor [microform] / Kevin Wilkes and Walter F. O'Brien, A. Karl Owen.
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[Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
1996
0 resources
Wave augmented diffusers for centrifugal compressors [microform] / Daniel E. Paxson, Gary J. Skoch.
Text
[Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
1998
0 resources
Effect of area ratio on the performance of a 5.5:1 pressure ratio centrifugal impeller [microform] / Lawrence F. Schumann, David A. Clark, and Jerry R. Wood.
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[Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, 1986]
1986
0 resources
Extended parametric representation of compressor fans and turbines [microform] / [G. L. Converse, R. G. Griffin].
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Cincinnati, Ohio : General Electric Company, Aircraft Engine Business Group, Advanced Technology Programs Dept. ; Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, [1984]
1984
0 resources
Computational study of the CC3 impeller and vaneless diffuser experiment / Sameer Kulkarni, Timothy A. Beach, Gary J. Skoch.
Text
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, September 2013.
2013-9
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo55298Aerodynamic performance of a compact, high work-factor centrifugal compressor at the stage and subcomponent level / Edward P. Braunscheidel [and four others].
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Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, September 2015.
2015-9
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo64050Forced response testing of anaxi-centrifugal turboshaft engine / A. Karl Owen [and three others].
Text
Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center ; Adelphi, Maryland : U.S. Army Research Laboratory, August 1996.
1996-8
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo69828Dynamic modeling of starting aerodynamics and stage matching in an axi-centrifugal compressor / Kevin Wilkes and Walter F. O'Brien, A. Karl Owen.
Text
Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center : U.S. Army Research Laboratory, October 1996.
1996-10
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo70387Progress of high efficiency centrifugal compressor simulations using TURBO / Sameer Kulkarni, Timothy A. Beach.
Text
Cleveland Ohio : National Aeronautics and Space Administration, Glenn Research Center, March 2017.
2017-3
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo79536Rotary-wing relevant compressor aero research and technology development activities at Glenn Research Center / Gerard E. Welch ... [and others].
Text
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
2012
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo29187No results found from Digital Research Books Beta
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