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Aerodynamic characteristics at supersonic speeds of a series of wing-body combinations having cambered wings with an aspect ratio of 3.5 and a taper ratio of 0.2 : effects of sweep angle and thickness ratio on the static lateral stability characteris

John H Hilton, M Leroy Spearman

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Key concepts: Wing, Supersonic speed, Aerodynamics, Series (stratigraphy), Aspect ratio (aeronautics), Swept wing, Structural engineering, Engineering

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Aerodynamic characteristics at supersonic speeds of a series of wing-body combinations having cambered wings with an aspect ratio of 3.5 and a taper ratio of 0.2 : effects of sweep angle and thickness ratio on the static lateral stability characteris — Research Paper | ScholarLens