K. SZEMA

Hypersonic Mach number and real gas effects on Space Shuttle Orbiteraerodynamics

J. R. Maus, B. J. GRIFFITH, K. SZEMA et al. · Journal of Spacecraft and Rockets · 1984 · 102 citations

Missile, Space Vehicle, Engineering +30

Application of a new class of high accuracy TVD schemes to the Navier-Stokes equations

S. R. Chakravarthy, K. SZEMA, Uriel Goldberg et al. · 23rd Aerospace Sciences Meeting · 1985 · 99 citations

Numerical Analysis, Aeroacoustics, Engineering +12

Chemical equilibrium laminar or turbulent three-dimensional viscous shock-layer flows

RAJIV THAREJA, K. SZEMA, C. LEWIS · Journal of Spacecraft and Rockets · 1983 · 27 citations

Missile, Space Vehicle, Engineering +26

A conservative type-dependent full potential method for the treatment of supersonic flows with embedded subsonic regions

V. S. Shankar Sriram, K. SZEMA, Stanley Osher · 1983 · 16 citations

Numerical Analysis, Aeroacoustics, Engineering +20

Viscous shock-layer predictions for hypersonic laminar or turbulent flows in chemical equilibrium over the windward surface of a Shuttle-like vehicle

RAJIV THAREJA, K. SZEMA, C. LEWIS · 20th Aerospace Sciences Meeting · 1982 · 16 citations

Unsteady Flow, Engineering, Turbulent Flows +9