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Viscous-shock-layer analysis of hypersonic flows over long slender vehicles [PDF]

open access: yes
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
core   +1 more source

Hypersonic turbulent quantities in support of Morkovin's hypothesis. [PDF]

open access: yesNat Commun
Segall BA   +6 more
europepmc   +1 more source

High-Reynolds-Number Turbulence Database: AeroFlowData. [PDF]

open access: yesSci Data
Zhang W   +18 more
europepmc   +1 more source

Weak wall boundary conditions for compressible flows. [PDF]

open access: yesEng Comput
Jaiswal M   +4 more
europepmc   +1 more source

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