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Aerodynamic characteristics in pitch of a modified half ring wing body combination and a swept wing body combination at Mach 2.16 to 3.70

Matthew James Lamb, Odell A. Morris

Abstract

Wind tunnel stability tests of pinch of modified half ring wing body and swept wing body combinations at supersonic speeds

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What this paper is about

Wind tunnel stability tests of pinch of modified half ring wing body and swept wing body combinations at supersonic speeds

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OpenAlex reports 4 citations for this work. Citation counts describe recorded attention and do not establish research quality.

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Available abstract

Wind tunnel stability tests of pinch of modified half ring wing body and swept wing body combinations at supersonic speeds

Key concepts: Wing, Aerodynamics, Mach number, Wing configuration, Wing twist, Structural engineering, Acoustics, Physics

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Aerodynamic characteristics in pitch of a modified half ring wing body combination and a swept wing body combination at Mach 2.16 to 3.70 — Research Paper | ScholarLens

Aerodynamic characteristics in pitch of a modified half ring wing body combination and a swept wing body combination at Mach 2.16 to 3.70

About this research paper

What this paper is about

Why it matters

Key contribution

Method / approach

Main findings

Limitations

Applications

Available abstract

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