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1
Preliminary design of turbopumps and related machinery /
by Wislicenus, George F. (George Friedrich), 1903-
[Cleveland, Ohio] : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1986

Government Document Book
2
Effect of rotor meridional velocity ratio on response to inlet radial and circumferential distortion /
by Sanger, Nelson L.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1979

Government Document Book
3
Analytical and experimental study of mean flow and turbulence characteristics inside the passages of an axial flow inducer /
by Gorton, C. A.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1980

Government Document Book
4
Aerodynamic performance of axial-flow fan stage operated at nine inlet guide vane angles /
by Moore, Royce D.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1979

Government Document Book
5
Forward acoustic performance of a model turbofan designed for a high specific flow (QF-14) /
by Lucas, James G.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1982

Government Document Book
6
Analytic investigation of effect of end-wall contouring on stator performance /
by Boyle, Robert J.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1981

Government Document Book
7
Analytical and experimental study of flow phenomena in noncavitating rocket pump inducers /
by Lakshminarayana, B.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1981

Government Document Book
8
GRID30-computer program for fast generation of multilevel, three-dimensional boundary-conforming o-type computational grids /
by Dulikravich, Djordje S.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1981

Government Document Book
9
Performance of single-stage axial-flow transonic compressor with rotor and stator aspect ratios of 1.63 and 1.77, respectively, and with design pressure ratio of 2.05 /
by Moore, Royce D.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1982

Government Document Book
10
Comparison of two- and three-dimensional flow computations with laser anemometer measurements in a transonic compressor rotor /
by Chima, Rodrick V.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1982

Government Document Book
11
Improved method for calculating transonic velocities on blade-to-blade stream surfaces of a turbomachine /
by Wood, Jerry R.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1981

Government Document Book
12
Damping seals for turbomachinery /
by Von Pragenau, George L.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1982

Government Document Book
13
Development of a locally mass flux conservative computer code for calculating 3-D viscous flow in turbomachines /
by Walitt, Leonard
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1982

Government Document Book
14
Aerodynamic effect of a honeycomb rotor tip shroud on a 50.8-centimeter-tip-diameter core turbine /
by Moffitt, Thomas P.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1983

Government Document Book
15
Aircraft noise prediction program user's manual /
by Gillian, Ronnie E.
Washington, D.C. : [Springfield, Va.] : U.S. National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1982

Government Document Book
16
Effects of diffusion factor, aspect ratio, and solidity on overall performance of 14 compressor middle stages /
by Britsch, Werner R.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1979

Government Document Book
17
Instability in rotating machinery : proceedings of a symposium /
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985

Government Document Book
18
A rapid perturbation procedure for determining nonlinear flow solutions : application to transonic turbomachinery flows /
by Stahara, Stephen S.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1981

Government Document Book
19
Performance of two-stage fan having low-aspect-ratio, first-stage rotor blading /
by Urasek, Donald C.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1979

Government Document Book
20
Aerodynamic performance of 1.38-pressure-ratio, variable-pitch fan stage /
by Moore, Royce D.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1979

Government Document Book
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