Zobrazeno 1 - 10
of 16
pro vyhledávání: '"Andrew B. Weaver"'
Publikováno v:
AIAA SCITECH 2022 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9ed4f39fa0f18ca72cb37cb3c46587e4
https://doi.org/10.2514/6.2022-2320
https://doi.org/10.2514/6.2022-2320
Autor:
Jeffrey S. West, Ranjan S. Mehta, Manuel P. Gale, Douglas G. Westra, Peter A. Liever, Andrew B. Weaver
Publikováno v:
Earth and Space 2021.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c0027576ebcbbd3a5ad56c17d709ab94
https://doi.org/10.1061/9780784483374.009
https://doi.org/10.1061/9780784483374.009
Publikováno v:
Journal of Thermophysics and Heat Transfer. 30:689-694
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3f49fc87fa00814d3862a51f414aab5c
https://doi.org/10.2514/1.t4780
https://doi.org/10.2514/1.t4780
Autor:
Iain D. Boyd, Andrew B. Weaver
Publikováno v:
AIAA SPACE 2016.
Unsteady, direct simulation Monte Carlo/particle-in-cell simulations of rocket plume expansions into the magnetosphere at geostationary Earth orbit are presented for three rocket thruster pulse dur...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::1bbdeceb17ce55f3d8d3d1d6845ee8a5
https://doi.org/10.2514/6.2016-5384
https://doi.org/10.2514/6.2016-5384
Publikováno v:
Journal of Thermophysics and Heat Transfer. 25:10-20
Uncertainty quantification in the hypersonic flow regime offers valuable information to determine physical models in need of improvement and to assist in design of vehicles and flight experiments. Here we present results of uncertainty quantification
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0f4baa9101c5e1fac220220d223368af
https://doi.org/10.2514/1.49522
https://doi.org/10.2514/1.49522
Publikováno v:
45th AIAA Thermophysics Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ec1245903ed5413131d8b6294b224263
https://doi.org/10.2514/6.2015-2352
https://doi.org/10.2514/6.2015-2352
Autor:
Andrew B. Weaver, Alina Alexeenko
Publikováno v:
School of Aeronautics and Astronautics Faculty Publications
The effect of molecular models on viscosity and thermal conductivity calculations is investigated. The Direct Simulation Monte Carlo (DSMC) method for rarefied gas flows is used to simulate Couette and Fourier flows as a means of obtaining the transp
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::4b58082c5a9574c984ae5ef6660926d8
http://docs.lib.purdue.edu/cgi/viewcontent.cgi?article=1047&context=aaepubs
http://docs.lib.purdue.edu/cgi/viewcontent.cgi?article=1047&context=aaepubs
Publikováno v:
44th AIAA Thermophysics Conference.
The forced harmonic oscillator (FHO) model is an attractive choice for implementation into DSMC due to its higher accuracy over the LarsenBorgnakke (L-B) model, and the fact that it is still an analytic expression. The higher accuracy comes with high
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::62eed4096c06f1890226e981e50cc61d
https://doi.org/10.2514/6.2013-2783
https://doi.org/10.2514/6.2013-2783
Autor:
Marc Adams, Alina Alexeenko, Andrew B. Weaver, Ares J. Rosakis, Marat Kulakhmetov, M Slipchenko, J. M. Mihaly
Publikováno v:
50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition.
Currently used hypersonic flow models, such as high-enthalpy reaction and energy relaxation rates, are based on experiments conducted at relatively low flow enthalpies and are highly uncertain. This paper presents analysis of the feasibility of calib
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::fcda8725a499b7781962bbcf9efaedca
https://doi.org/10.2514/6.2012-596
https://doi.org/10.2514/6.2012-596
Publikováno v:
48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition.
Uncertainty quantification (UQ) in the hypersonic flow regime offers valuable information to determine physical models in need of improvement and to assist in design of vehicles and flight experiments. Here we present results of UQ analysis based on
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::af210409af13e1e10c78f1d355da7efa
https://doi.org/10.2514/6.2010-1180
https://doi.org/10.2514/6.2010-1180