NASA VG V/STOL Fighters Studies from the early 1960s

flateric

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Static longitudinal and lateral aerodynamic characteristics at a Mach number of 2.20 of a V STOL airplane configuration with a variable-sweep wing and with a skewed wing design


TM-X-521
"STATIC LONGITUDINAL AND LATERAL AERODYNAMIC CHARACTERISTICS AT A MACH NUMBER OF 2.20 OF A V/STOL AIRPLANE CONFIGURATION WITH A VARIABLE-SWEEP WING AND WITH A SKEWED WING DESIGN"
 

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flateric

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flateric

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More pics of third configuration
 

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hesham

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