Showing 1 - 11 results of 11 for search '', query time: 0.14s Refine Results
  1. 1
    Experimental investigation to validate use of cryogenic temperatures to achieve high Reynolds numbers in boattail pressure testing /
    by Reubush, David E.
    Published 1976
    Government Document Book
  2. 2
    Effect of Reynolds number on the aerodynamic stability and control characteristics of a 55 degree clipped-delta-wing orbiter configuration at supersonic Mach numbers /
    by Blair, A. B.
    Published 1976
    Government Document Book
  3. 3
    A study of the sonic-boom characteristics of a blunt body at a Mach number of 4.14 /
    by Carlson, Harry W., Mack, Robert J.
    Published 1977
    Government Document Book
  4. 4
    Supersonic nonlinear potential flow analysis : interim report /
    by Siclari, Michael J.
    Published 1984
    Government Document Book
  5. 5
    Supersonic through-flow fan design /
    Published 1987
    Government Document Book
  6. 6
    Application of advanced computational codes in the design of an experiment for a supersonic throughflow fan rotor /
    Published 1987
    Government Document Book
  7. 7
    Numerical analysis of supersonic flow through oscillating cascade sections by using a deforming grid /
    by Huff, Dennis L.
    Published 1989
    Government Document Book
  8. 8
    Numerical simulations of supersonic flow through oscillating cascade sections /
    by Huff, Dennis L.
    Published 1990
    Government Document Book
  9. 9
    Screech noise source structure of a supersonic rectangular jet /
    by Rice, Edward J.
    Published 1992
    Government Document Book
  10. 10
    Supersonic reacting internal flow fields.
    by Drummond, J. Philip
    Published 1990
    Government Document Microform Book
  11. 11
    Subsonic, transonic, and supersonic nozzle flow by the inverse technique /
    Book
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