Zobrazeno 1 - 9
of 9
pro vyhledávání: '"Reynaldo J. Gomez"'
Autor:
William A. Wood, Reynaldo J. Gomez, Kyle B. Thompson, Karen L. Bibb, Michael A. Park, Steffan H. Tesch, William L. Kleb
Publikováno v:
AIAA Aviation 2019 Forum.
Numerical simulation of the Reynolds-averaged Navier–Stokes (RANS) equations has become a critical tool for the design of aerospace vehicles. However, the issues that affect the grid convergence of three dimensional RANS solutions are not completel
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::910431e0b9e83315a3278b8ba8d7fd60
https://doi.org/10.2514/6.2019-2948
https://doi.org/10.2514/6.2019-2948
Publikováno v:
AIAA Aviation 2019 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d16bc2f6116bc1f6b9859095306fdb73
https://doi.org/10.2514/6.2019-3397
https://doi.org/10.2514/6.2019-3397
Autor:
Jeremy T. Pinier, Reynaldo J. Gomez, Floyd J. Wilcox, Stuart E. Rogers, Derek J. Dalle, David T. Chan
Publikováno v:
54th AIAA Aerospace Sciences Meeting.
The development of the aerodynamic database for the Space Launch System (SLS) booster separation environment has presented many challenges because of the complex physics of the ow around three independent bodies due to proximity e ects and jet inter-
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::68e47c2aa49ba923b779066209895523
https://doi.org/10.2514/6.2016-0798
https://doi.org/10.2514/6.2016-0798
Autor:
John R. Campbell, Reynaldo J. Gomez, John Blevins, David W. Bennett, Russ D. Rausch, Cetin C. Kiris
Publikováno v:
52nd Aerospace Sciences Meeting.
Aerodynamic environments are some of the rst engineering data products that are needed to design a space launch vehicle. These products are used in performance predic- tions, vehicle control algorithm design, as well as determing loads on primary and
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1c013aaa6be0857ecc440261b5f4c131
https://doi.org/10.2514/6.2014-1253
https://doi.org/10.2514/6.2014-1253
Autor:
Curtis E. Larsen, Luc Huyse, Phillip C. Stuart, David S. Riha, Chris Waldhart, Reynaldo J. Gomez, M. Asce
Publikováno v:
48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference.
On Feb 1, 2003, the Shuttle Columbia was lost during its return to Earth. As a result of the conclusion that debris impact caused the damage to the left wing of the Columbia Space Shuttle Vehicle (SSV) during ascent, the Columbia Accident Investigati
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3169419993e7b82bdb8ad3d8c1dff498
https://doi.org/10.2514/6.2007-1954
https://doi.org/10.2514/6.2007-1954
Autor:
Phillip C. Stuart, Jason B. Pleming, Luc Huyse, Reynaldo J. Gomez, David S. Riha, Ben H. Thacker
Publikováno v:
47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference 14th AIAA/ASME/AHS Adaptive Structures Conference 7th.
As a result of the conclusion that debris impact caused the damage to the left wing of the Columbia Space Shuttle Launch Vehicle (SSLV) during ascent, the Columbia Accident Investigation Board (CAIB) recommended that an assessment be performed of the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e070e96d29119cb8145d48e718e026b3
https://doi.org/10.2514/6.2006-1778
https://doi.org/10.2514/6.2006-1778
Publikováno v:
22nd Applied Aerodynamics Conference and Exhibit.
A collection of computational fluid dynamics tools and techniques are being developed and tested for application to stage separation and abort simulation for next-generation launch vehicles. In this work, an overset grid Navier-Stokes flow solver has
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a394f5941a64bf294370e1fecad14319
https://doi.org/10.2514/6.2004-4838
https://doi.org/10.2514/6.2004-4838
Autor:
Stuart E. Rogers, Darby Vicker, William M. Chan, Michael J. Aftosmis, Scott M. Murman, Robert L. Meakin, Moffett Field, Reynaldo J. Gomez
Publikováno v:
34th AIAA Fluid Dynamics Conference and Exhibit.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0d487bef99ad1c4f428c158e4caeb962
https://doi.org/10.2514/6.2004-2226
https://doi.org/10.2514/6.2004-2226
Autor:
Reynaldo J. Gomez, William M. Chan
Publikováno v:
14th Computational Fluid Dynamics Conference.
A ,scheme is described for .the automatic domain decomposition .and creation of overset grids around surface discontinuities. Curves along surface discontinuities are called seam curves. The seam curves are first automatically‘extracted from a mult
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e2c22da73d0160cbeec4b539f4208689
https://doi.org/10.2514/6.1999-3303
https://doi.org/10.2514/6.1999-3303