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.
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