Showing 1 - 6 results of 6 for search 'Robins, A. Warner', query time: 0.03s Refine Results
  1. 1
    Aerodynamic characteristics at Mach numbers of 1.5, 1.8, and 2.0 of a blended wing-body configuration with and without integral canards /

    Aerodynamic characteristics at Mach numbers of 1.5, 1.8, and 2.0 of a blended wing-body configuration with and without integral canards / by Robins, A. Warner

    Published 1979
    Search for the full-text version of this title in HathiTrust
    Government Document Book
    Save to List
    Saved in:
  2. 2
    Supersonic wings with significant leading-edge thrust at cruise /

    Supersonic wings with significant leading-edge thrust at cruise / by Robins, A. Warner

    Published 1982
    Search for the full-text version of this title in HathiTrust
    Government Document Book
    Save to List
    Saved in:
  3. 3
    A method for the determination of the time lag in pressure measuring systems incorporating capillaries /

    A method for the determination of the time lag in pressure measuring systems incorporating capillaries / by Sinclair, Archibald R.

    Published 1952
    Other Authors: “…Robins, A. Warner…”
    Government Document Book
    Save to List
    Saved in:
  4. 4
    Concept development of a Mach 3.0 high-speed civil transport

    Concept development of a Mach 3.0 high-speed civil transport

    Published 1988
    Other Authors: “…Robins, A. Warner…”
    Government Document Microfilm Book
    Save to List
    Saved in:
  5. 5
    Longitudinal aerodynamic characteristics of an elliptical body with a horizontal tail at mach numbers 2.3 to 4.63 /

    Longitudinal aerodynamic characteristics of an elliptical body with a horizontal tail at mach numbers 2.3 to 4.63 / by Shrout, Barrett L.

    Published 1982
    Other Authors: “…Robins, A. Warner…”
    Search for the full-text version of this title in HathiTrust
    Government Document Book
    Save to List
    Saved in:
  6. 6
    Preliminary performance of a vertical-attitude takeoff and landing, supersonic-cruise aircraft concept having thrust vectoring integrated into the flight control system

    Preliminary performance of a vertical-attitude takeoff and landing, supersonic-cruise aircraft concept having thrust vectoring integrated into the flight control system

    Published 1985
    Other Authors: “…Robins, A. Warner…”
    Government Document Microfilm Book
    Save to List
    Saved in:
Search Tools: RSS Feed – Save Search