Zobrazeno 1 - 10
of 12
pro vyhledávání: '"Khalil Bensassi"'
Publikováno v:
International Journal for Numerical Methods in Fluids. 94:941-975
Autor:
Brett A. Cruden, E Papajak, Amal Sahai, Khalil Bensassi, Augustin Tibere-Inglesse, Aaron M. Brandis, David Schwenke, Christopher O. Johnston
Publikováno v:
AIAA SCITECH 2023 Forum.
Publikováno v:
AIAA SCITECH 2022 Forum.
Publikováno v:
International Journal of Heat and Mass Transfer. 113:889-897
In order to investigate the accuracy of the rebuilding code for the free stream conditions and the total enthalpy in the Longshot Hypersonic facility at the von Karman Institute (VKI), a series of unsteady CFD simulations of axisymmetric hypersonic f
Autor:
Aaron M. Brandis, Khalil Bensassi
Publikováno v:
AIAA Scitech 2019 Forum.
Numerical investigations of the flowfield inside NASA Ames' Electric Arc Shock Tube have been performed. The focus is to simulate the experiments designed to reproduce shock layer radiation layer relevant to Earth re-entry conditions. This paper asse
Publikováno v:
Proceedings of the 32nd International Symposium on Shock Waves (ISSW32 2019).
Time accurate simulation of non-equilibrium flows inside shock tube facilities presents several challenges from both physical and mathematical aspects. Furthermore, the drastic computational cost makes it non-practical to support real-time experiment
Publikováno v:
43rd Fluid Dynamics Conference.
Reynolds-averaged Navier-Stokes (RANS) turbulence models have been widely used for simulating hypersonic turbulent boundary layers, without any specific considerations regarding the thermochemical nonequilibrium effects. In most hypersonic solvers th
Publikováno v:
21st AIAA Computational Fluid Dynamics Conference.
Publikováno v:
51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition.
Pitot pressure surveys of the Longshot hypersonic contoured nozzle in the von Karman Institute are presented. Measurements use a rake of pitot probes at four locations along the nozzle axis from half the nozzle length down to the exit. Laminar and tu
Publikováno v:
Scopus-Elsevier
Numerical simulations of hypersonic ows using local correlation based transition (LCTM) model was performed in order to assess the accuracy of the model in hypersonic conditions. Implementation of the model was done in object oriented framework. The