D. E. Fetterman
Abstract
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Investigation of half-cone delta wing configurations under laminar boundary layer conditions at Mach 6.86 to determine favorable interference effects on maximum lift-drag ratio
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Investigation of half-cone delta wing configurations under laminar boundary layer conditions at Mach 6.86 to determine favorable interference effects on maximum lift-drag ratio
Key concepts: Drag, Drag divergence Mach number, Lift-induced drag, Mach number, Delta wing, Lift (data mining), Interference (communication), Mechanics