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Effects of Deflected Wing Tips on the Aerodynamic Characteristics of a Canard Configuration at Mach Numbers from 0.7 to 3.5

Loren G Bright, Victor L. Peterson

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Abstract

Aerodynamic characteristics of canard configuration at subsonic and supersonic speeds with deflected wing tips for longitudinal and directional stability

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What this paper is about

Aerodynamic characteristics of canard configuration at subsonic and supersonic speeds with deflected wing tips for longitudinal and directional stability

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Available abstract

Aerodynamic characteristics of canard configuration at subsonic and supersonic speeds with deflected wing tips for longitudinal and directional stability

Key concepts: Aerodynamics, Mach number, Wing, Aerospace engineering, Wing configuration, Aeronautics, Engineering, Physics

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Effects of Deflected Wing Tips on the Aerodynamic Characteristics of a Canard Configuration at Mach Numbers from 0.7 to 3.5 — Research Paper | ScholarLens