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

Schueller, Carl F Stitt, Leonard E
naca-rm-e56k28b
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:
http://naca.central.cranfield.ac.uk/reports/1957/naca-rm-e56k28b.pdf