A uniformly valid solution for the three-dimensional inviscid supersonic flow past blunt bodies with strong compression in the shock wave
DOI10.1007/BF01176511zbMath0517.76066OpenAlexW2043460950MaRDI QIDQ1053551
Publication date: 1982
Published in: Acta Mechanica (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1007/bf01176511
streamlinesthree dimensionalsteadyblunt bodiesdensity ratio across shock very smallflow quantitiesfreestream momentum flux normal to body surfacehypersonic similarity parameterparaboloidal or hyperboloidal shapespressure does not change along normal to shock surfacesharp nosed
Shock waves and blast waves in fluid mechanics (76L05) Supersonic flows (76J20) Hypersonic flows (76K05)
Cites Work
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- Supersonic flow past a bluff body with a detached shock Part I Two-dimensional body
- On the theory of hypersonic flow past plane and axially symmetric bluff bodies
- Calculation of the influence of centrifugal forces on surface pressure for a body of arbitrary shape in hypersonic flow
- A uniformly valid solution for the hypersonic flow past blunted bodies
- Surface geometry of three-dimensional inviscid hypersonic flows.
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