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  1. 1

    Basic helicopter aerodynamics by Seddon, J.

    Washington, DC : London, UK : American Institute of Aeronautics and Astronautics ; Blackwell Scientific Publications, 1990
    Format: Book


  2. 2

    Identification and verification of frequency-domain model for XV-15 tilt-rotor aircraft dynamics by Tischler, Mark B.

    Moffett Field, Calif. : St. Louis, Mo. : National Aeronautics and Space Administration, Ames Research Center ; U.S. Army Aviation Systems Command, 1984
    Format: Government Document Book


  3. 3

    Calculation of the distributed loads on the blades of individual multiblade propellers in axial flow using linear and nonlinear lifting surface theories by Pesetskaya, N. N.

    Washington, DC : National Aeronautics and Space Administration, 1988
    Format: Government Document Book


  4. 4

    Computation of transonic potential flow about three-dimensional inlets, ducts, and bodies by Reyhner, Theodore A.

    Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1982
    Format: Government Document Book


  5. 5

    Einführung in die theoretische Gasdynamik. by Sauer, R. (Robert), 1898-1970

    Berlin : Springer, 1951
    2. Aufl.
    Format: Book


  6. 6

    Aerodynamic characteristics of a 1/6-scale powered model of the rotor systems research aircraft by Mineck, Raymond E.

    Washington : Springfield, Va. : National Aeronautics and Space Administration ; For sale by the National Technical Information Service, 1977
    Format: Government Document Book


  7. 7

    Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 8t̊o 90 ̊

    Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [For sale by the National Technical Information Service], 1979
    Format: Government Document Book


  8. 8

    Some recent advances in computational aerodynamics for helicopter applications by McCroskey, W. J.

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


  9. 9

    A hybrid numerical technique for predicting the aerodynamic and acoustic fields of advanced turboprops final report by Homicz, G. F.

    Buffalo, N.Y. : Arvin Calspan Advanced Technology Center, 1985
    Format: Government Document Book


  10. 10

    Aircraft propulsion, theory and performance ; an introductory text book for students of aeronautics. by Morley, Arnold William

    London, New York : Longmans Green, 1953
    Format: Book


  11. 11

    A review of 50 years of aerodynamic research with NACA/NASA by Spearman, M. Leroy

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


  12. 12

    Statistical analysis of atmospheric turbulence about a simulated block building by Steely, Sidney L.

    Washington : [Springfield, Va.] :; Washington : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [for sale by the National Technical Information Service],; National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1980
    Format: Government Document Book


  13. 13

    An investigation of the ability to recover from transients following failures for single-pilot rotorcraft by Mansur, M. Hossein

    Moffett Field, Calif. : [Springfield, Va. : National Aeronautics and Space Administration, Ames Research Center : US Army Aviation Systems Command, Aviation Research and Technology Activity ; For sale by the National Technical Information Service, 1988
    Format: Government Document Book


  14. 14

    An investigation of the flow characteristics in the blade endwall corner region by Hazarika, Birinchi K.

    [Washington, DC] : National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987
    Format: Government Document Book


  15. 15

    Fundamentals of hydro- and aeromechanics. by Tietjens, Oskar Karl Gustav, 1893-

    New York ; London : McGraw-Hill book company, inc., 1934
    1st ed.
    Format: Book


  16. 16

    Low Reynolds number aerodynamics : proceedings of the conference, Notre Dame, Indiana, USA, 5-7 June 1989

    Berlin ; New York : Springer-Verlag, 1989
    Format: Conference Proceeding Book


  17. 17

    Inverse boundary-layer theory and comparison with experiment by Carter, James E. (James Edward), 1944-

    [Washington] : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information Service, 1978
    Format: Government Document Book


  18. 18

    User's manual for AeroFcn : a FORTRAN program to compute aerodynamic parameters by Conley, Joseph L.

    Edwards, Calif. : [Springfield, Va.] : National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility ; [For sale by the National Technical Information Service], 1992
    Format: Government Document Book


  19. 19

    Aerodynamic design trends for commercial aircraft by Hilbig, R.

    Washington D.C. : National Aeronautics and Space Administration, 1986
    Format: Government Document Book


  20. 20

    Theory of wing sections, including a summary of airfoil data, by Abbott, Ira H. A.

    New York, Dover Publications 1959
    Format: Book