Influence of the velocity gradient on the stagnation point heating in hypersonic flow

DOI10.1007/BF01419002zbMath0859.76035OpenAlexW2032983230MaRDI QIDQ1815771

Yanyan Li

Publication date: 15 April 1997

Published in: Shock Waves (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/bf01419002

zbMATH Keywords

integral methodconservation equationstangential velocity gradientreal gas effects

Mathematics Subject Classification ID

Hypersonic flows (76K05)

Cites Work

• An improved method to determine free stream conditions in hypersonic facilities
• On the theory of hypersonic flow past plane and axially symmetric bluff bodies
• Flow with a detached shock wave about a symmetrical profile
• Non-equilibrium dissociating nitrogen flow over spheres and circular cylinders
• Static pressure distribution in the free turbulent jet
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