An inlet design concept to reduce flow distortion at angle of attack

Schueller, Carl F Stitt, Leonard E
February 26, 1957

Flow distortions were measured at the inlet face and diffuser exit of three axisymmetric inlets operating at angles of attack of 0 degree to 14 degrees and at a Mach number of 1.91.

An Adobe Acrobat (PDF) file of the entire report: