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Displaying 1-18 of 18 results
Multistage simulations of the GE90 turbine [microform] / Mark G. Turner ... [et al.].
- Text
- [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
- 1999
MATE program. Volume II [microform] : erosion resistant compressor airfoil coating / Melvin Freling.
- Text
- [Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1987]
- 1987
Experimental/analytical approach to understanding mistuning in a transonic wind tunnel compressor [microform] / Teri Kaiser ... [et al.].
- Text
- Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
- 1994
Advanced turboprop wing installation effects measured by unsteady blade pressure and noise [microform] / Laurence J. Heidelberg and Richard P. Woodward ; prepared for the 11th Aeroacoustics Conference sponsored by the American Institute of Aeronautics and Astronautics, Sunnyvale, California, October 19-21, 1987.
- Text
- [Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1987]
- 1987
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
[Thin film strain gage development program] [microform] : [final program].
- Text
- [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1983]
- 1983
Structural tailoring of engine blades (STAEBL), theoretical manual [microform] / K.W. Brown.
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1986]
- 1986
Structural tailoring of engine blades (STAEBL), user's manual [microform] / K.W. Brown.
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1986]
- 1986
The measurement of boundary layers on a compressor blade in cascade at high positive incidence angle. II, Data report [microform] / Steve Deutsch and William C. Zierke.
- Text
- [Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1986]
- 1986
The measurement of boundary layers on a compressor blade in cascade at high positive incidence angle. I, Experiment techniques and results [microform] / Steve Deutsch and William C. Zierke.
- Text
- [Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1986]
- 1986
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
The effect of adding roughness and thickness to a transonic axial compressor rotor [microform] / Kenneth L. Suder ... [et al.].
- Text
- [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
- 1995
Development of a fiber optic compressor blade sensor [microform] : final report / principal investigator, Harbans Singh Dhadwal.
- Text
- [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
- 1995
Comparison of calculated and experimental cascade performance for controlled-diffusion compressor stator blading [microform] / Nelson L. Sanger and Raymond P. Shreeve.
- Text
- [Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, 1986]
- 1986
Secondary flow spanwise deviation model for the stators of NASA middle compressor stages [microform] / William B. Roberts and Donald M. Sandercock.
- Text
- Cleveland, Ohio : Lewis Research Center, [1984]
- 1984
The boundary layer on compressor cascade blades [microform] / submitted by Steven Deutsch and William C. Zierke.
- Text
- State College, PA : Applied Research Laboratory, The Pennsylvania State University ; [Washington, D.C. : National Aeronautics and Space Administration, 1986]
- 1986
Design procedures for compressor blades [microform] / H. Starken.
- Text
- Washington, DC : National Aeronautics and Space Administration, [1983]
- 1983
A model to assess the risk of ice accretion due to ice crystal ingestion in a turbofan engine and its effects on performance / Philip C. E. Jorgenson [and three others].
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, November 2013.
- 2013-11
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo53739
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