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Results of rocket model test of an airplane configuration having an arrow wing and slender flat-sided fuselage: lift, drag, longitudinal stability, lateral force, and jet effects at Mach numbers between 1.0 and 2.3

Description: Report presenting testing of a rocket-propelled model of an airplane with an arrow wing with a 55 degree leading-edge sweep and a flat-sided fuselage mounting swept horizontal and vertical tails using the pulsed-control technique at a range of Mach numbers. Results regarding longitudinal trim, lift and stability, drag, lateral force, and thrust and jet effects are provided.
Date: February 21, 1956
Creator: Peck, Robert F.
Partner: UNT Libraries Government Documents Department