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Sideslip characteristics at various angles of attack for several hypersonic missile configurations with canard controls at a Mach number of 2.01

Gerald V. Foster

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Abstract

Lateral and longitudinal aerodynamic characteristics of hypersonic missile configurations with canard controls in supersonic pressure tunnel

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Lateral and longitudinal aerodynamic characteristics of hypersonic missile configurations with canard controls in supersonic pressure tunnel

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Available abstract

Lateral and longitudinal aerodynamic characteristics of hypersonic missile configurations with canard controls in supersonic pressure tunnel

Key concepts: Mach number, Hypersonic speed, Aerospace engineering, Missile, Angle of attack, Aeronautics, Physics, Engineering

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Sideslip characteristics at various angles of attack for several hypersonic missile configurations with canard controls at a Mach number of 2.01 — Research Paper | ScholarLens