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2020•AIAA JournalRequires access

Correction: Experimental Investigation of Two Hypersonic Shock Turbulent Boundary Layer Interactions

Anne-Marie Schreyer, Dipankar Sahoo, Owen J. H. Williams, Alexander John Smits

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Abstract

Correction

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What this paper is about

Correction

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Method / approach

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Available abstract

Correction

Key concepts: Hypersonic speed, Boundary layer, Shock (circulatory), Mechanics, Turbulence, Physics, Aerospace engineering, Engineering

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Correction: Experimental Investigation of Two Hypersonic Shock Turbulent Boundary Layer Interactions — Research Paper | ScholarLens