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Jet effects on cylindrical afterbodies housing sonic and supersonic nozzles which exhaust against a supersonic stream at angles of attack from 90 degree to 180 degree [NASA TN D-1016]

By: Hayman,Jr, Lovick O.
Contributor(s): Mcdearmon,Russell W.
Material type: materialTypeLabelBookSeries: National Aeronaitics and Space Adminstration ; NASA technical note. Publisher: Washington, D.C. National aeronautics and space adminstraion 1962Description: 47p.Subject(s): Cylindrical afterbodies
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