Suggested Topics within your search.
Showing 1 - 20 results of 163 for search '', query time: 0.07s Refine Results
  1. 1
    Spin-tunnel investigation to determine the effectiveness of a rocket for spin recovery /

    Spin-tunnel investigation to determine the effectiveness of a rocket for spin recovery / by Neihouse, A. I.

    Published 1949
    Search for the full-text version of this title in HathiTrust
    Government Document Book
    Save to List
    Saved in:
  2. 2
    Floating characteristics of rudders and elevators in spinning attitudes as determined from hinge-moment-coefficient data with application to personal-owner-type airplanes /

    Floating characteristics of rudders and elevators in spinning attitudes as determined from hinge-moment-coefficient data with application to personal-owner-type airplanes / by Bihrle, William

    Published 1950
    Government Document Book
    Save to List
    Saved in:
  3. 3
    Pilot escape from spinning airplanes as determined from free-spinning-tunnel tests /

    Pilot escape from spinning airplanes as determined from free-spinning-tunnel tests / by Scher, Stanley H.

    Published 1951
    Government Document Book
    Save to List
    Saved in:
  4. 4
    Floating characteristics of a plain and a horn-balanced rudder at spinning attitudes as determined from rotary tests on a model of a typical low-wing personal-owner airplane /

    Floating characteristics of a plain and a horn-balanced rudder at spinning attitudes as determined from rotary tests on a model of a typical low-wing personal-owner airplane / by Bihrle, William

    Published 1951
    Search for the full-text version of this title in HathiTrust
    Government Document Book
    Save to List
    Saved in:
  5. 5
    The aerodynamic forces and moments on a 1/10-scale model of a fighter airplane in spinning attitudes as measured on a rotary balance in the Langley 20-foot free-spinning tunnel /

    The aerodynamic forces and moments on a 1/10-scale model of a fighter airplane in spinning attitudes as measured on a rotary balance in the Langley 20-foot free-spinning tunnel / by Stone, Ralph W., Jr

    Published 1950
    Government Document Book
    Save to List
    Saved in:
  6. 6
    Spin-tunnel investigation of the effects of mass and dimensional variations on the spinning characteristics of a low-wing single-vertical-tail model typical of personal-owner airplanes /

    Spin-tunnel investigation of the effects of mass and dimensional variations on the spinning characteristics of a low-wing single-vertical-tail model typical of personal-owner airpl... by Klinar, Walter J. (Walter Jacob)

    Published 1951
    Search for the full-text version of this title in HathiTrust
    Government Document Book
    Save to List
    Saved in:
  7. 7
    Comparison of model and full-scale spin recoveries obtained by use of rockets /

    Comparison of model and full-scale spin recoveries obtained by use of rockets / by Burk, Sanger M.

    Published 1954
    Government Document Book
    Save to List
    Saved in:
  8. 8
    Aerodynamic characteristics of airplanes at high angles of attack /

    Aerodynamic characteristics of airplanes at high angles of attack / by Chambers, Joseph R.

    Published 1977
    Government Document Book
    Save to List
    Saved in:
  9. 9
    Spin-tunnel investigation to determine the effect on spin recoveries of reducing the opening shock load of spin-recovery parachutes /

    Spin-tunnel investigation to determine the effect on spin recoveries of reducing the opening shock load of spin-recovery parachutes / by Jones, Ira P.

    Published 1950
    Government Document Book
    Save to List
    Saved in:
  10. 10
    Side forces on a tangent ogive forebody with a fineness ratio of 3.5 at high angles of attack and Mach numbers from 0.1 to 0.7 /

    Side forces on a tangent ogive forebody with a fineness ratio of 3.5 at high angles of attack and Mach numbers from 0.1 to 0.7 /

    Published 1977
    Search for the full-text version of this title in HathiTrust
    Government Document Book
    Save to List
    Saved in:
  11. 11
    Characteristics of two sharp-nosed airfoils having reduced spinning tendencies /

    Characteristics of two sharp-nosed airfoils having reduced spinning tendencies / by Jacobs, Eastman N. (Eastman Nixon), 1902-1987

    Published 1932
    Online Access
    Government Document eBook
    Save to List
    Saved in:
  12. 12
    SPINEQ, a program for determining aircraft equilibrium spin characteristics including stability /

    SPINEQ, a program for determining aircraft equilibrium spin characteristics including stability / by Adams, William M.

    Published 1978
    Search for the full-text version of this title in HathiTrust
    Government Document Book
    Save to List
    Saved in:
  13. 13
    Analysis of a spin and recovery from time histories of attitudes and velocities as determined for a dynamic model of a contemporary fighter airplane in the free-spinning tunnel /

    Analysis of a spin and recovery from time histories of attitudes and velocities as determined for a dynamic model of a contemporary fighter airplane in the free-spinning tunnel / by Scher, Stanley H.

    Published 1956
    Government Document Book
    Save to List
    Saved in:
  14. 14
    Free-spinning-tunnel investigation of gyroscopic effects of jet-engine rotating parts (or of rotating propellers) on spin and spin recovery /

    Free-spinning-tunnel investigation of gyroscopic effects of jet-engine rotating parts (or of rotating propellers) on spin and spin recovery / by Bowman, James S. (James Scarboro), 1924-

    Published 1955
    Government Document Book
    Save to List
    Saved in:
  15. 15
    Attitude determination of the spin-stabilized Project Scanner spacecraft /

    Attitude determination of the spin-stabilized Project Scanner spacecraft / by Walsh, T. M., Keating, Jean C., Hinton, Dwayne E.

    Published 1968
    Online Access
    Government Document eBook
    Save to List
    Saved in:
  16. 16
    Study of motion of model of personal-owner or liaison airplane through the stall and into the incipient spin by means of a free-flight testing technique /

    Study of motion of model of personal-owner or liaison airplane through the stall and into the incipient spin by means of a free-flight testing technique / by Stone, Ralph W., Jr

    Published 1953
    Government Document Book
    Save to List
    Saved in:
  17. 17
    Comparison of model and full-scale spin test results for 60 airplane designs /

    Comparison of model and full-scale spin test results for 60 airplane designs / by Berman, Theodore

    Published 1950
    Government Document Book
    Save to List
    Saved in:
  18. 18
    All about stalls & spins /

    All about stalls & spins / by Gentry, Everett

    Published 1983
    Book
    Save to List
    Saved in:
  19. 19
    Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 8̊to 90̊ /

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

    Published 1979
    Search for the full-text version of this title in HathiTrust
    Government Document Book
    Save to List
    Saved in:
  20. 20
    Rotation in free fall of rectangular wings of elongated shape /

    Rotation in free fall of rectangular wings of elongated shape / by Dupleich, Paul

    Published 1949
    Government Document Book
    Save to List
    Saved in:
Search Tools: RSS Feed – Save Search