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  1. 1
    An examination of the aerodynamic moment on rotor blade tips using flight test data and analysis

    An examination of the aerodynamic moment on rotor blade tips using flight test data and analysis by Maier, Thomas H.

    Moffett Field, Calif. : [Springfield, Va.] : US Army Aviation and Troop Command : National Aeronautics and Space Administration, Ames Research Center ; [National Technical Information Service, distributor], 1993
    Format: Government Document Book


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  2. 2
    Flutter analysis of supersonic axial flow cascades using a high resolution euler solver. Part 1, Formulation and validation

    Flutter analysis of supersonic axial flow cascades using a high resolution euler solver. Part 1, Formulation and validation

    Washington, DC : National Aeronautics and Space Administration, 1992
    Format: Government Document Book


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  3. 3
    Implementation and validation of a wake model for vortex-surface interactions in low-speed forward flight : semi-annual status report, period 10/1/86 - 3/31/87

    Implementation and validation of a wake model for vortex-surface interactions in low-speed forward flight : semi-annual status report, period 10/1/86 - 3/31/87 by Komerath, Narayanan M.

    [Washington, D.C.] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1987
    Format: Government Document Book


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  4. 4
    Energy efficient engine low pressure subsystem flow analysis

    Energy efficient engine low pressure subsystem flow analysis

    [Cleveland, Ohio] : Springfield, VA :; [Cleveland, Ohio] : Springfield, VA : National Aeronautics and Space Administration, Lewis Research Center ; National Technical Information Service, [distributor],; National Aeronautics and Space Administration, Lewis Research Center ; National Technical Information Service [distributor], 1998
    Format: Government Document Book


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  5. 5
    Integrated Technology Rotor Methodology Assessment Workshop : proceedings of a workshop

    Integrated Technology Rotor Methodology Assessment Workshop : proceedings of a workshop

    Moffett Field, Calif. : [Washington, D.C.?] : [Springfield, Va.?] : US Army Aviation Systems Command, Aviation Research and Technology Activity ; National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [National Technical Information Service, distributor], 1988
    Format: Government Document Conference Proceeding Book


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  6. 6
    Computational fluid dynamics study of the variable-pitch split-blade fan concept

    Computational fluid dynamics study of the variable-pitch split-blade fan concept by Kepler, C. E.

    [Washington, D.C.] : [Springfield, Va.] : National Aeronautics and Space Administration ; [National Technical Information Service, distributor], 1992
    Format: Government Document Book


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  7. 7
    Aeroacoustic codes for rotor harmonic and BVI noise - CAMRAD. Mod1/HIRES : methodology and users' manual

    Aeroacoustic codes for rotor harmonic and BVI noise - CAMRAD. Mod1/HIRES : methodology and users' manual

    Hampton, Va. : [Springfield, Va.] :; Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1998
    Format: Government Document Book


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  8. 8
    Three-dimensional flow field measurements in a transonic turbine

    Three-dimensional flow field measurements in a transonic turbine

    [Washington, DC] : [Springfield, Va.] :; [Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration : U.S. Army Research Laboratory ; [National Technical Information Service, distributor], 1996
    Format: Government Document Book


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  9. 9
    Linear and nonlinear dynamic analysis of redundant load path bearingless rotor systems

    Linear and nonlinear dynamic analysis of redundant load path bearingless rotor systems by Murthy, V. R.

    Moffett Field, Calif. : [Springfield, Va.] : National Aeronautics and Space Administration, Ames Research Center ; [National Technical Information Service, distributor], 1985
    Format: Government Document Book


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  10. 10
    An experimental and analytical method for approximate determination of the tilt rotor research aircraft rotor-wing download : final report, 05-30-94 - 11-30-85

    An experimental and analytical method for approximate determination of the tilt rotor research aircraft rotor-wing download : final report, 05-30-94 - 11-30-85 by Jordan, David E.

    San Luis Obispo, Calif. : [Washington, DC] : [Springfield, Va.] : California Polytechnic State University, Aeronautical Engineering Dept. ; [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1986
    Format: Government Document Book


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  11. 11
    Off-design computer code for calculating the aerodynamic performance of axial-flow fans and compressors : user's manual

    Off-design computer code for calculating the aerodynamic performance of axial-flow fans and compressors : user's manual by Schmidt, James F.

    [Washington, D.C.] : [Springfield, Va.] : National Aeronautics and Space Administration ; [National Technical Information Service, distributor], 1995
    Format: Government Document Book


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  12. 12
    Computation of helicopter rotor acoustics in forward flight

    Computation of helicopter rotor acoustics in forward flight by Strawn, Roger C. (Roger Clayton)

    [Moffett Field, Calif.] : [Springfield, Va.] : Research Institute for Advanced Computer Science, NASA Ames Research Center ; [National Technical Information Service, distributor], 1994
    Format: Government Document Book


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  13. 13
    Nonlinear (time domain) and linearized (title & freqency domain) solutions to the compressible Euler equations in conservation law form : final report for NASA Lewis Research Center

    Nonlinear (time domain) and linearized (title & freqency domain) solutions to the compressible Euler equations in conservation law form : final report for NASA Lewis Research Cente... by Sreenivas, Kidambi

    Mississippi States, MS : [Washington, D.C.] : [Springfield, Va.] : Computational Fluid Dynamics Laboratory, Engineering Research Center for Computational Field Simulation, Mississippi State University ; [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1995
    Format: Government Document Book


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  14. 14
    Aeroelastic model helicopter rotor testing in the Langley TDT

    Aeroelastic model helicopter rotor testing in the Langley TDT

    Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1985
    Format: Government Document Book


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  15. 15
    A mathematical simulation model of a CH-47B helicopter

    A mathematical simulation model of a CH-47B helicopter by Weber, Jeanine M., Liu, Tung Y., Chung, William

    Moffett Field, Calif. :; Moffett Field, California : National Aeronautics and Space Administration, Ames Research Center, 1984
    Format: Government Document Book


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  16. 16
    Full-scale hingeless rotor performance and loads

    Full-scale hingeless rotor performance and loads by Peterson, Randall L.

    Moffett Field, Calif. : [Springfield, Va.] : National Aeronautics and Space Administration, Ames Research Center ; [National Technical Information Service, distributor], 1995
    Format: Government Document Book


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  17. 17
    Aeroelastic simulation of higher harmonic control

    Aeroelastic simulation of higher harmonic control by Robinson, Lawson H.

    Moffett Field, Calif. : [Springfield, Va.] : National Aeronautics and Space Administration, Ames Research Center ; [National Technical Information Service, distributor], 1994
    Format: Government Document Book


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  18. 18
    Source methodology for turbofan noise prediction (SOURCED3D technical documentation)

    Source methodology for turbofan noise prediction (SOURCED3D technical documentation) by Meyer, Harold D.

    [Cleveland, Ohio] : Springfield, VA : National Aeronautics and Space Administration, Glenn Research Center ; National Technical Information Service, distributor, 1999
    Format: Government Document Book


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  19. 19
    A study of helicopter stability and control including blade dynamics

    A study of helicopter stability and control including blade dynamics by Zhao, Xin, 1955-

    [Princeton, N.J.] : [Washington, D.C.] : [Springfield, Va.] : Princeton University, Dept. of Mechanical nad Aerospace Engineering ; [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1988
    Format: Government Document Book


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  20. 20
    A numerical model for dynamic wave rotor analysis

    A numerical model for dynamic wave rotor analysis by Paxson, Daniel E.

    [Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration ; [National Technical Information Service, distributor], 1995
    Format: Government Document Book


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