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An investigation at Mach numbers from 0.40 to 1.00 of a model with a wing having inboard sections cambered for Mach 1.2

R. J. Re, Gunar Stumbris

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Abstract

Longitudinal aerodynamic characteristics of wing body tail combination at high subsonic speeds

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Longitudinal aerodynamic characteristics of wing body tail combination at high subsonic speeds

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Method / approach

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Available abstract

Longitudinal aerodynamic characteristics of wing body tail combination at high subsonic speeds

Key concepts: Mach number, Wing, Geology, Aerospace engineering, Physics, Computer science, Mechanics, Engineering

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An investigation at Mach numbers from 0.40 to 1.00 of a model with a wing having inboard sections cambered for Mach 1.2 — Research Paper | ScholarLens

An investigation at Mach numbers from 0.40 to 1.00 of a model with a wing having inboard sections cambered for Mach 1.2

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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