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Zero-lift Drag of a Large Fuselage Cavity and a Partially Submerged Store on a 52.5 Degree Sweptback-wing - Body Configuration as Determined from Free-flight Tests at Mach Numbers of 0.7 to 1.53

Sherwood Hoffman

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Key concepts: Fuselage, Wing, Mach number, Lift (data mining), Lift-to-drag ratio, Angle of attack, Drag, Physics

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Zero-lift Drag of a Large Fuselage Cavity and a Partially Submerged Store on a 52.5 Degree Sweptback-wing - Body Configuration as Determined from Free-flight Tests at Mach Numbers of 0.7 to 1.53 — Research Paper | ScholarLens