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Effects of Wing Planform on the Aerodynamic Characteristics of a Wing-body-tail Model at Mach Numbers 1.57, 2.16, and 2.87

L. S. Jernell, R. L. Mc Kinney

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Abstract

Aerodynamic characteristics of swept wing configuration with progressive series of leading and trailing edge modifications

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What this paper is about

Aerodynamic characteristics of swept wing configuration with progressive series of leading and trailing edge modifications

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Available abstract

Aerodynamic characteristics of swept wing configuration with progressive series of leading and trailing edge modifications

Key concepts: Wing, Planform, Aerodynamics, Mach number, Wing loading, Wing twist, Environmental science, Aerospace engineering

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Effects of Wing Planform on the Aerodynamic Characteristics of a Wing-body-tail Model at Mach Numbers 1.57, 2.16, and 2.87 — Research Paper | ScholarLens