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Multistage simulations of the GE90 turbine [microform] / Mark G. Turner ... [et al.].
Microform
[Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
1999
0 resources
Comparison of calculated and experimental cascade performance for controlled-diffusion compressor stator blading [microform] / Nelson L. Sanger and Raymond P. Shreeve.
Microform
[Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, 1986]
1986
0 resources
Secondary flow spanwise deviation model for the stators of NASA middle compressor stages [microform] / William B. Roberts and Donald M. Sandercock.
Microform
Cleveland, Ohio : Lewis Research Center, [1984]
1984
0 resources
The boundary layer on compressor cascade blades [microform] / submitted by Steven Deutsch and William C. Zierke.
Microform
State College, PA : Applied Research Laboratory, The Pennsylvania State University ; [Washington, D.C. : National Aeronautics and Space Administration, 1986]
1986
0 resources
Design procedures for compressor blades [microform] / H. Starken.
Microform
Washington, DC : National Aeronautics and Space Administration, [1983]
1983
0 resources