Numerical simulation of the lateral aerodynamics of an orbital stage at stage separation flow conditions

DOI10.1016/S1270-9638(00)00132-2zbMath0977.76055OpenAlexW2011465694WikidataQ127097586 ScholiaQ127097586MaRDI QIDQ4500545

Christian Breitsamter, Boris Laschka, Tomislav Cvrlje

Publication date: 18 January 2001

Published in: Aerospace Science and Technology (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/s1270-9638(00)00132-2

zbMATH Keywords

unsteady aerodynamicsaerodynamic characteristicsEuler solverAUSM schemelateral motionthree-dimensional unsteady Euler equationsexplicit finite volume methodflexible multiblock grid generatortwo-stage hypersonic vehicletwo-stage separation

Mathematics Subject Classification ID

Finite volume methods applied to problems in fluid mechanics (76M12) Hypersonic flows (76K05)

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