Lateral Stability Characteristics Between Mach Numbers Of 0 80 And 1 57 And Simulation Of Coupled Motion At Mach Number Of 1 30 Of A Rocket Propelled Model Of An Airplane Configuration Having Thin Highly Tapered 45 Degree Sweptback Surfaces
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Lateral Stability Characteristics Between Mach Numbers of 0.80 and 1.57 and Simulation of Coupled Motion at Mach Number of 1.30 of a Rocket-propelled Model of an Airplane Configuration Having Thin Highly Tapered 45 Degree Sweptback Surfaces
A rocket-propelled model of an airplane configuration having thin, highly tapered, 45 degree sweptback surfaces was tested in the Mach number range of 0.80 to 1.57 to obtain the lateral stability characteristics of the configuration.
Lateral Stability Investigation at Mach Numbers from 0.8 to 1.7 of Two Rocket-boosted Models of an Airplane Configuration with a 45 Degree Swept Wing and a Low Horizontal Tail
Rocket-boosted free-flight tests of two models of an airplane configuration having a 45 degree swept wing and a low horizontal-tail position have provided lateral stability derivatives and control effectiveness data for a Mach number range from 0.8 to 1.7. The experimental lateral stability derivatives presented are corrected to rigid conditions and compared with theoretically calculated rigid derivatives. The results are presented without detailed analysis.