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    Delta wings with shock-free cross flow (1984)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: In order to have a high level of maneuverability, supersonic delta wings should have a cross flow that is free of embedded shock waves. The conical cross flow sonic surface differs from that of plane transonic flow in many aspects. Well-known properties such as the monotone law are not true for conical cross flow sonic surfaces. By using a local analysis of the cross flow sonic line, relevant conditions for smooth cross flow are obtained. A technique to artificially construct a smooth sonic surface and an efficient numerical method to calculate the flow field are used to obtain cones with smooth cross flow.
    Keywords: AERODYNAMICS
    Type: NASA-CR-172297 , NAS 1.26:172297 , REPT-84-6
    Format: application/pdf
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