Results of Rocket Model Test of an Airplane Configuration Having an Arrow Wing and Slender Flat-sided Fuselage PDF Download

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Results of Rocket Model Test of an Airplane Configuration Having an Arrow Wing and Slender Flat-sided Fuselage

Results of Rocket Model Test of an Airplane Configuration Having an Arrow Wing and Slender Flat-sided Fuselage PDF Author: Robert F. Peck
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 26

Book Description
A rocket-propelled model of an airplane configuration having an arrow wing with 55 degree leading-edge sweep and a flat-sided fuselage mounting swept horizontal and vertical tails has been tested through use of the pulse-control technique at Mach numbers between 1.0 and 2.3. Results are presented from an investigation of longitudinal trim, lift, stability, drag, lateral force, thrust, and jet effects.
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