Hypersonic slender-wedge analysis with gradual change in angle of attack

DOI10.1007/BF01176505zbMath0555.76050OpenAlexW2082909716MaRDI QIDQ761311

D. Kharzeev

Publication date: 1983

Published in: Acta Mechanica (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/bf01176505

zbMATH Keywords

angle of attack changing exponentially with timeslender two-dimensional wedge-wings

Mathematics Subject Classification ID

Hypersonic flows (76K05)

Cites Work

• Comment on "Controllability Limit of a Human Pilot"
• Low-frequency, large-amplitude fluctuations of the laminar boundary layer.
• Unnamed Item

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