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Effect of hypersonic research engine installation on aerodynamic characteristics of 0.0667-scale model of X-15A-2 airplane at Mach numbers from 1.75 to 4.63

E. B. Graves

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Abstract

Wind tunnel stability tests to determine effect of hypersonic research engine on aerodynamic characteristics of research aircraft

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What this paper is about

Wind tunnel stability tests to determine effect of hypersonic research engine on aerodynamic characteristics of research aircraft

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OpenAlex reports 1 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 to determine effect of hypersonic research engine on aerodynamic characteristics of research aircraft

Key concepts: Airplane, Aerodynamics, Mach number, Aerospace engineering, Aeronautics, Scale (ratio), Engineering, Hypersonic speed

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Effect of hypersonic research engine installation on aerodynamic characteristics of 0.0667-scale model of X-15A-2 airplane at Mach numbers from 1.75 to 4.63 — Research Paper | ScholarLens