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Martin, A. W.

Publications and source records attributed to Martin, A. W..

Investigation of normal shock inlets for highly maneuverable aircraft

Concepts are investigated for obtaining both low cowl drag and good inlet performance at high angles of attack. The effect of a canard on inlet performance for a kidney shaped inlet in each of two vertical locations is discussed along with a sharp lip two dimensional inlet on a canardless forebody.

Martin, A. W.