Supersonic-tunnel tests of two supersonic airplane model configurations

Macon C. Ellis, Jr., Lowell E. Hasel, Carl E. Grigsby
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.

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