Supersonic-tunnel tests of two supersonic airplane model configurations

Macon C. Ellis, Jr., Lowell E. Hasel, Carl E. Grigsby
naca-rm-l7j15
Dec 1947


Supersonic-tunnel tests of two models of similar supersonic airplane configurations were made at Mach numbers of 1.55, 1.90, and 2.32 to determine values of the drag, lift, pitching moment, yawing moment, and side force.

An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1947/naca-rm-l7j15.pdf