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Radial and circumferential flow surveys at the inlet and exit of the Space Shuttle Main Engine High Pressure Fuel Turbine model [microform] / S.T. Hudson ... [et al.].
Microform
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Collection efficiency and ice accretion calculations for a Boeing 737-300 inlet [microform] / Colin S. Bidwell.
Microform
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
1997
0 resources
Dynamic simulation of a wave rotor topped turboshaft engine [microform] / R.B. Greendyke, D.E. Paxson, M.T. Schobeiri.
Microform
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
1997
0 resources
Estimating engine airflow in gas-turbine powered aircraft with clean and distorted inlet flows [microform] / J.G. Williams and W.G. Steenken, A.J. Yuhas.
Microform
Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
1996
0 resources
The high stability engine control (HISTEC) program [microform] : flight demonstration phase / John C. DeLaat ... [et al.].
Microform
[Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
1998
0 resources
Parametric data from a wind tunnel test on a rocket-based combined-cycle engine inlet [microform] / René Fernandez ... [et al.].
Microform
[Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2001]
2001
1 resource
Available online
Adobe Acrobat Reader requiredDesign and development of an F/A-18 inlet distortion rake [microform] : a cost and time saving solution / Andrew J. Yuhas ... [et al.].
Microform
[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : For sale by the National Technical Information Service, 1995]
1995
1 resource
Available online
http://purl.access.gpo.gov/GPO/LPS60790Two-phase flows and heat transfer within systems with ambient pressure above the thermodynamic critical pressure [microform] / R. C. Hendricks, M. J. Braun, R. L. Mullen.
Microform
[Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, 1986]
1986
1 resource
Available online
http://purl.access.gpo.gov/GPO/LPS84436V/STOL model fan rig, design report [microform] / [ J. G. Cheatham, T. L. Creason].
Microform
[Washington, D.C.] : National Aeronautics and Space Administration, [1983]
1983
0 resources
Analysis of buzz in a supersonic inlet / Rodrick V. Chima.
Web Resource
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
2012
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo30597Effects of spent cooling and swirler angle on a 9-point swirl-venturi injector / Zhuohui J. He [and four others].
Web Resource
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, April 2014.
2014-4
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo54279Collection efficiency and ice accretion calculations for a Boeing 737-300 inlet / Colin S. Bidwell.
Web Resource
Cleveland, Ohio : National National Aeronautics and Space Administration, Lewis Research Center, February 1997.
1997-2
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo70396Dynamic simulation of a wave rotor topped turboshaft engine / R.B. Greendyke, D.E. Paxson, M.T. Schobeiri.
Web Resource
Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, July 1997.
1997-7
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo73175Parametric data from a wind tunnel test on a rocket-based combined-cycle engine inlet / René Fernandez [and three others].
Web Resource
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, November 2001.
2001-11
1 resource
Available online
https://purl.fdlp.gov/GPO/LPS26716NASA numerical and experimental evaluation of UTRC low emissions injector / Yolanda R. Hicks [and five others].
Web Resource
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, September 2014.
2014-9
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo56698No results found from Digital Research Books Beta
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