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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
ntrs.nasa.gov
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"
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 - NASA Technical Reports Server (NTRS)
Static longitudinal and lateral aerodynamic characteristics of V/STOL aircraft with variable sweep wing
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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