Zobrazeno 1 - 10
of 13
pro vyhledávání: '"Gerald J. LeBeau"'
Autor:
Forrest E. Lumpkin, Gerald J. LeBeau
Publikováno v:
Computer Methods in Applied Mechanics and Engineering. 191:595-609
The DSMC Analysis Code (DAC) software represents the National Aeronautics and Space Administration's (NASA's) state-of-the-art implementation of the Direct Simulation Monte Carlo (DSMC) method of Bird for simulating three-dimensional flows. It is uti
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5b43d4fa94d49247129f6f0af756a184
https://doi.org/10.1016/s0045-7825(01)00304-8
https://doi.org/10.1016/s0045-7825(01)00304-8
Publikováno v:
Journal of Spacecraft and Rockets. 37:39-48
The nozzle and plume ows of small cold-gas attitude control thrusters, plume interactions with spacecraft surfaces, and the induced pressure environment are investigated numerically. The motivation for this study originates from pressure measureme
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ce8e982a4591a5e795c9cc9b38331abf
https://doi.org/10.2514/2.3547
https://doi.org/10.2514/2.3547
Publikováno v:
Journal of Spacecraft and Rockets. 34:8-15
Acceleration data taken for the e rst time from the orbital acceleration research experiment during re-entry on Space Transportation System-62 have been analyzed using in situ calibration factors. The re-entry data include the e ight regime from orbi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::16a78974396542cc67e8b5966dc49b67
https://doi.org/10.2514/2.3183
https://doi.org/10.2514/2.3183
Publikováno v:
AIP Conference Proceedings.
Plume impingement effects from the descent and ascent engine firings of the Lunar Lander were analyzed in support of the Lunar Architecture Team under the Constellation Program. The descent stage analysis was performed to obtain shear and pressure fo
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::810b8f932e27877d14515138980d8d9d
https://doi.org/10.1063/1.3562711
https://doi.org/10.1063/1.3562711
Publikováno v:
AIP Conference Proceedings.
Plume impingement effects on the Orion Crew Service Module (CSM) were analyzed for various dual Reaction Control System (RCS) engine firings and various configurations of the solar arrays. The study was performed using a decoupled computational fluid
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ca5f9066a02f747a28297028e0be8174
https://doi.org/10.1063/1.3562712
https://doi.org/10.1063/1.3562712
Publikováno v:
AIP Conference Proceedings.
Three‐dimensional Direct Simulation Monte Carlo simulations of Columbia Shuttle Orbiter flight STS‐107 are presented. The aim of this work is to determine the aerodynamic and heating behavior of the Orbiter during aerobraking maneuvers and to pro
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::18236eac1839f890b37e24607777de94
https://doi.org/10.1063/1.1941698
https://doi.org/10.1063/1.1941698
Publikováno v:
37th AIAA Thermophysics Conference.
Three-dimensional Direct Simulation Monte Carlo simulations of Columbia Shuttle Orbiter flight STS-107 are presented. The aim of this work is to determine the aerodynamic and heating behavior of the Orbiter during aerobraking maneuvers and to provide
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ef719d589985ba33f60c15588c737770
https://doi.org/10.2514/6.2004-2282
https://doi.org/10.2514/6.2004-2282
The Use of Virtual Sub-cells in DSMC Analysis of Orbiter Aerodynamics at High Altitudes Upon Reentry
Publikováno v:
41st Aerospace Sciences Meeting and Exhibit.
o reduce the cell size constraint of the method on the flowfield cells. While the benefits of virtual sub -cells have been demonstrated on an idealized two - dimensional problem, the goal of this work is to investigate their effectiveness on a challe
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c948f1b4fd4ba213bfb956be5d26118b
https://doi.org/10.2514/6.2003-1030
https://doi.org/10.2514/6.2003-1030
Publikováno v:
AIP Conference Proceedings.
This paper presents the results of a numerical study of shock interactions resulting from Mach 10 air flow about a sharp double cone. Computations are made with the direct simulation Monte Carlo (DSMC) method by using two different codes: the G2 code
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::dce214832980864083d5c5b43292f061
https://doi.org/10.1063/1.1581578
https://doi.org/10.1063/1.1581578
Publikováno v:
38th Aerospace Sciences Meeting and Exhibit.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e5aae9aefe0ce59c4bb6e16cec98ac12
https://doi.org/10.2514/6.2000-462
https://doi.org/10.2514/6.2000-462