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Effects of wing planform on the aerodynamic characteristics of a wing-body-tail model at Mach numbers from 1.70 to 4.63

L. S. Jernell

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Abstract

Effects of wing planform on aerodynamic characteristics in pitch and sideslip of wing-body-tail model at supersonic wind tunnel speeds

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Effects of wing planform on aerodynamic characteristics in pitch and sideslip of wing-body-tail model at supersonic wind tunnel speeds

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Available abstract

Effects of wing planform on aerodynamic characteristics in pitch and sideslip of wing-body-tail model at supersonic wind tunnel speeds

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

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Effects of wing planform on the aerodynamic characteristics of a wing-body-tail model at Mach numbers from 1.70 to 4.63 — Research Paper | ScholarLens