Boundary-layer viscous correction method for hypersonic forebody/inlet integration

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Hydrogen fuel rocket engines simulation using LOGOS code

N. N. Smirnov, R.M. Shagaliev, I.M. Belyakov et al. · International Journal of Hydrogen Energy · 2014 · 522 citations

Engineering, Aerospace Engineering, Mechanical Engineering +14

Influences of the turbulence model and the slot width on the transverse slot injection flow field in supersonic flows

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Engineering, Aerospace Engineering, Physics +11

Review and assessment of turbulence models for hypersonic flows

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Engineering, Aerospace Engineering, Physics +14

Design of Three-Dimensional Hypersonic Inlets with Rectangular-to-Elliptical Shape Transition

Michael K. Smart · Journal of Propulsion and Power · 1999 · 252 citations · Full text

Engineering, Aerospace Engineering, Mechanical Engineering +17