Effect of Reynolds number on the aerodynamic stability and control characteristics of a 55 ÌŠclipped-delta-wing orbiter configuration at supersonic mach ... (NASA technical memorandum, NASA TM X-3376)

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Effect of Reynolds number on the aerodynamic stability and control characteristics of a 55 ÌŠclipped-delta-wing orbiter configuration at supersonic mach ... (NASA technical memorandum , NASA TM X-3376) (ID: B0006WALM4)	Description and Photos \| More ads in Aircraft

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Effect of Reynolds number on the aerodynamic stability and control characteristics of a 55 ÌŠclipped-delta-wing orbiter configuration at supersonic mach ... (NASA technical memorandum , NASA TM X-3376)

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