Browsing by Author "Robinson, A."

Browsing by Author "Robinson, A."

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  • Wave reflection near a wall 
    Robinson, A. (College of Aeronautics, Cranfield., 1950-05)
    The field of flow due to a shock wave or explanation wave undergoes a considerable modification in the neighbourhood of a rigid wall. It has been suggested that the resulting propagation of the disturbance upstream is ...
  • Wing body interference at supersonic speeds 
    Kirkby, S.; Robinson, A. (College of Aeronautics, Cranfield, 1947-04)
    The increment in lift due to wing-body interference at supersonic speed is calculated approximately for an untapered wing without sweepback.