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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

Clyde V. Hamilton

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Abstract

A change in Mach number .from1.60 t o 2.01 had l i t t l e e f f e c t on C but.-.increased the positive-values of C I .

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A change in Mach number .from1.60 t o 2.01 had l i t t l e e f f e c t on C but.-.increased the positive-values of C I .

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Available abstract

A change in Mach number .from1.60 t o 2.01 had l i t t l e e f f e c t on C but.-.increased the positive-values of C I .

Key concepts: Supersonic speed, Wing, Aspect ratio (aeronautics), Aerodynamics, Mach number, Overall pressure ratio, Series (stratigraphy), Angle of attack

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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