Viscous-shock-layer analysis of hypersonic flows over long slender vehicles [PDF]
An efficient and accurate method for solving the viscous shock layer equations for hypersonic flows over long slender bodies is presented. The two first order equations, continuity and normal momentum, are solved simultaneously as a coupled set. The flow
Gupta, Roop N., Lee, Kam-Pui
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Research on Star Sensor Imaging Simulation Under Near-Space Hypersonic Non-Equilibrium Flow Conditions. [PDF]
Liao Z +7 more
europepmc +1 more source
Kinetic Theory-Based Methods in Fluid Dynamics. [PDF]
Chen Z, Zhang L, Yang L.
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Hypersonic turbulent quantities in support of Morkovin's hypothesis. [PDF]
Segall BA +6 more
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Non-ideal gas behavior matters in hydrodynamic instability. [PDF]
Ren J, Kloker M.
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Experimental study of nose-tip bluntness effects on hypersonic boundary-layer transition in a shock tunnel. [PDF]
Kim J, Nam J, Hur J, Kim J, Lee BJ.
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Nonlinear Modeling Study of Aerodynamic Characteristics of an X38-like Vehicle at Strong Viscous Interaction Regions. [PDF]
Jiang D, Wang P, Li J, Mao M.
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High-Reynolds-Number Turbulence Database: AeroFlowData. [PDF]
Zhang W +18 more
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Adaptive physics-informed neural operator for coarse-grained non-equilibrium flows. [PDF]
Zanardi I, Venturi S, Panesi M.
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Weak wall boundary conditions for compressible flows. [PDF]
Jaiswal M +4 more
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