Browsing by Author "Robinson, A."

Browsing by Author "Robinson, A."

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  • Source and vortex distributions in the linearised theory of steady supersonic flow 
    Robinson, A. (College of Aeronautics, Cranfield, 1947-10)
    The hyperbolic character of the differential equation satisfied by the velocity potential in linearised supersonic flow entails the presence of fractional infinities in the fundamental solutions of the equation. Difficulties ...
  • 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.