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Design and performance of controlled diffusion stator compared with original double-circular-arc stator / Thomas F. Gelder [and others].
Microform
[Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va.] : [National Technical Information Service, distributor], [1989]
1989
0 resources
Dynamics of rotating multi-component turbomachinery systems / Charles Lawrence.
Microform
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va.] : [For sale by the National Technical Information Service], [1993]
1993
0 resources
Propfan test assessment propfan propulsion system static test report / D.M. O'Rourke.
Microform
Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va.] : [For sale by the National Technical Information Service], [1987]
1987
0 resources
Aeroelastic response and stability of tiltrotors with elastically-coupled composite rotor blades / Mark W. Nixon.
Microform
[Washington, DC] : [National Aeronautics and Space Administration] ; [Springfield, Va.] : [National Technical Information Service, distributor], [1993]
1993
0 resources
Interim report on the experimental and analytical investigation of fan flow interaction with downstream struts : interim report #1 for the period June 16, 1984 to March 15, 1985 / T.L. Olsen, W.F. Ng, W.F. O'Brien.
Microform
[Hampton, Va.] : National Aeronautics and Space Administration, Langley Research Center, [1985]
1985
0 resources
Unsteady analysis of rotor blade tip flow / B. Maskew and B.M. Rao.
Microform
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : National Technical Information Service, distributor, 1985.
1985
0 resources
The effect of adding roughness and thickness to a transonic axial compressor rotor / Kenneth L. Suder [and others].
Microform
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va.] : [National Technical Information Service, distributor], [1995]
1995
0 resources
Study of controlled diffusion stator blading II [microform] : final report / R.F. Behlke, J.D. Brooky and E. Canal.
Microform
Cleveland, Ohio : National Aeronautics and Space Administration, NASA-Lewis Research Center, [1983]
1983
0 resources
Highly loaded compressor with boundary layer suction / par Klaus Hubrich.
Manuscript
2005.
2005
1 item
Call number | JSD 07-110 |
Item location | Offsite |
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
Design procedures for compressor blades [microform] / H. Starken.
Microform
Washington, DC : National Aeronautics and Space Administration, [1983]
1983
0 resources
Comparison between measured turbine stage performance and the predicted performance using quasi-3D flow and boundary layer analyses [microform] / Robert J. Boyle and Jeffrey E Haas and Theodore Katsanis.
Microform
[Washington, D.C. : National Aeronautics and Space Administration, 1984]
1984
0 resources
Redesign and cascade tests of a supercritical controlled diffusion stator blade-section [microform] / James F. Schmidt, Thomas F. Gelder, and Leo F. Donovan.
Microform
[Washington, D.C. : National Aeronautics and Space Administration, 1984]
1984
0 resources
Off-design performance loss model for radial turbines with pivoting, variable-area stators / Peter L. Meitner, Arthur J. Glassman.
Web resource
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, November 1980.
1980
1 resource
Available online
Effects of tip clearance on overall performance of transonic fan stage with and without casing treatment / Royce D. Moore and Walter M. Osborn.
Web resource
Washington, D.C. : National Aeronautics and Space Administration, February 1977.
1977
1 resource
Available online
An aerodynamic analysis of a single-bladed rotor in hovering and low-speed forward flight as determined from smoke studies of the vorticity distribution in the wake.
Book/text
1957.
1957
1 item
Call number | PRIN 685 1957 .25 |
Item location | Off-site |