1974•AIAA JournalOpen access
Shock Wave Boundary-Layer Interactions in Laminar Transonic Flow
H. BRILLIANT, T. C. Adamson
Open full text 25 citations
Abstract
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H. BRILLIANT, T. C. Adamson
Abstract
Open-access reader
Peer Reviewed
OpenAlex reports 25 citations for this work. Citation counts describe recorded attention and do not establish research quality.
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Peer Reviewed
Key concepts: Boundary layer, Laminar flow, Transonic, Mechanics, Shock wave, Flow separation, Shock (circulatory), Subsonic and transonic wind tunnel