The asymptotic structure of weak shock waves in flows over symmetrical bodies at Mach number unity
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Publication:2531836
DOI10.1007/BF01178831zbMath0172.52901MaRDI QIDQ2531836
Publication date: 1968
Published in: Acta Mechanica (Search for Journal in Brave)
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Nonlinear effects in steady supersonic dissipative gasdynamics. Part 2. Three-dimensional axisymmetric flow ⋮ Transonic equivalence rule: a nonlinear problem involving lift
Cites Work
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- Leading Edge of a Shock-Induced Boundary Layer
- Stabilitätsgebiete eines speziellen zweiparametrigen Systems von zwei Differentialgleichungen 2. Ordnung mit periodischen Koeffizienten
- Structure of Weak Non-Hugoniot Shocks
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