An investigation of the effects of nose and lip shapes for an underslung scoop inlet at Mach numbers from 0 to 1.9

Pfyl, Frank A
naca-rm-a55g13
November 18, 1955

No Abstract Available

An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1955/naca-rm-a55g13.pdf