Zobrazeno 1 - 10
of 15
pro vyhledávání: '"Sami D. Habchi"'
Publikováno v:
Journal of Spacecraft and Rockets. 48:93-102
A numerical investigation is presented for hypersonic rocket exhaust plume flow over lunar surface, a problem offering limited experimental data and significant challenges to computational models in practice. In this paper, examinations on the accura
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ce16e440885edd52ebd1ae2166ca3a95
https://doi.org/10.2514/1.50813
https://doi.org/10.2514/1.50813
Publikováno v:
AIAA Journal. 48:2157-2164
An efficient solver for the velocity―vorticity form of the Navier―Stokes equations on adaptive Cartesian grids is presented. The excessive numerical dissipation common to most grid-based Navier―Stokes solvers is avoided by solving the fluid dyn
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9c79719d51d6992952768833466b857a
https://doi.org/10.2514/1.j050472
https://doi.org/10.2514/1.j050472
Publikováno v:
Journal of Spacecraft and Rockets. 40:632-638
Flowfield solutions over the Beagle 2 Mars probe aeroshell, spanning the trajectory through the Martian atmosphere, have been generated for the continuum flow regime for Mach numbers from 1.5 to 28 at angles of attack from 0 to 11 deg. Static aerodyn
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::24c80b3da46537bb2c7cf17726f5fca4
https://doi.org/10.2514/2.6911
https://doi.org/10.2514/2.6911
Publikováno v:
50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a5170b9b4a659d74e99466e482505ad3
https://doi.org/10.2514/6.2012-800
https://doi.org/10.2514/6.2012-800
Publikováno v:
AIAA Journal. 32:936-941
The selection of primary dependent variables for the solution of Navier-Stokes equations in the curvilinear body-fitted coordinates is still an unsettled issue. Reported formulations with primitive variables involve contravariant velocity components,
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::984bc8104ed5f2f6587da3419ce7fa8e
https://doi.org/10.2514/3.12077
https://doi.org/10.2514/3.12077
Publikováno v:
48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition.
An efficient solver for the velocity-vorticity form of the Navier-Stokes equations on adaptive Cartesian grids is presented. The excessive numerical dissipation common to most grid-based Navier-Stokes solvers is avoided by solving the fluid dynamic e
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4fce7cfab3302914781aa83f920b1e4e
https://doi.org/10.2514/6.2010-1072
https://doi.org/10.2514/6.2010-1072
Publikováno v:
46th AIAA Aerospace Sciences Meeting and Exhibit.
Morphing technology enables aerospace vehicles to achieve a broader range of operational modes. Computational aeroelastic and design analysis tools of these vehicles must be able to handle arbitrarily large deformations and shape changes. The objecti
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8c763549a7bc1ca641a5cd331f70b208
https://doi.org/10.2514/6.2008-677
https://doi.org/10.2514/6.2008-677
Publikováno v:
36th AIAA Fluid Dynamics Conference and Exhibit.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d22a3ffdd4de45b9e00772b0df2703b9
https://doi.org/10.2514/6.2006-3205
https://doi.org/10.2514/6.2006-3205
Publikováno v:
36th AIAA Fluid Dynamics Conference and Exhibit.
Modern aerospace vehicles that operate at high angles of attack and perform aggressive maneuvers are subject to several dynamic loads problems such as buffet and flutter. Accurate model-based simulation of these problems requires careful attention to
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::62b90efc00a26cc6b992f6a88e23cace
https://doi.org/10.2514/6.2006-3219
https://doi.org/10.2514/6.2006-3219
Autor:
Peter A. Liever, Sami D. Habchi
Publikováno v:
22nd Applied Aerodynamics Conference and Exhibit.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c5d15636719049ca5ffb2b01ea3cd69b
https://doi.org/10.2514/6.2004-4726
https://doi.org/10.2514/6.2004-4726