On the theory of hypersonic flow past plane and axially symmetric bluff bodies
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Publication:3236890
DOI10.1017/S0022112056000226zbMath0071.40702MaRDI QIDQ3236890
Publication date: 1956
Published in: Journal of Fluid Mechanics (Search for Journal in Brave)
Related Items (8)
Analytical solution of a problem of a collision of two hypersonic gas flows from symmetric sources ⋮ A model of supersonic flow past blunt axisymmetric bodies, with application to Chester's solution ⋮ The boundary layer near the stagnation point in hypersonic flow past a sphere ⋮ Numerical simulation of supersonic flow past reentry capsules ⋮ Calculation of the influence of centrifugal forces on surface pressure for a body of arbitrary shape in hypersonic flow ⋮ A Lagrangian formulation for steady three-dimensional Newton-Busemann flow ⋮ Influence of the velocity gradient on the stagnation point heating in hypersonic flow ⋮ A uniformly valid solution for the three-dimensional inviscid supersonic flow past blunt bodies with strong compression in the shock wave
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