Research Catalog

  • Performance of an aerodynamic yaw controller mounted on the space shuttle orbiter body flap at Mach 10 [microform] / W.I. Scallion.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995
  • Effects of nozzle exit geometry and pressure ratio on plume shape for nozzles exhausting into quiescent air [microform] / W.I. Scallion.

    • Text
    • Hamtpon, Va. : National Aeronautics and Space Administration, Langley Research Center : [Springfield, Va. : For sale by the National Technical Information Service, 1991]
    • 1991
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS60070

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