Showing 1 - 8 results of 8 for search 'Pittman, Jimmy L.', query time: 0.18s Refine Results
  1. 1
    Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts at Mach numbers of 2.96, 3.96, and 4.63 /
    by Pittman, Jimmy L.
    Published 1980
    Government Document Book
  2. 2
    Application of supersonic linear theory and hypersonic impact methods to three nonslender hypersonic airplane concepts at mach numbers from 1.10 to 2.86 /
    by Pittman, Jimmy L.
    Published 1979
    Government Document Book
  3. 3
    Body and canard effects on an attached-flow maneuver wing at Mach 1.62 /
    by Pittman, Jimmy L.
    Published 1984
    Government Document Book
  4. 4
    Supersonic, nonlinear, attached-flow wing design for high lift with experimental validation /
    by Pittman, Jimmy L.
    Published 1984
    Government Document Book
  5. 5
    Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts at Mach numbers of 2.96, 3.96, and 4.63 /
    Get full text
    Government Document eBook
  6. 6
    Aerodynamic characteristics at Mach numbers from 0.33 to 1.20 of wing-body design concept for a hypersonic research airplane /
    by Dillon, James L.
    Published 1977
    Other Authors: “...Pittman, Jimmy L....”
    Government Document Book
  7. 7
    Aerodynamic characteristics at Mach 6 of a wing-body concept for a hypersonic research airplane /
    by Dillon, James L.
    Published 1978
    Other Authors: “...Pittman, Jimmy L....”
    Government Document Book
  8. 8
    Aerodynamic characteristics of a hypersonic cruise aircraft concept with wing-mounted propulsion systems at mach numbers of 2.96, 3.96, and 4.63 /
    by Riebe, Gregory D.
    Published 1981
    Other Authors: “...Pittman, Jimmy L....”
    Government Document Book
Search Tools: RSS Feed – Email Search