Zobrazeno 1 - 7
of 7
pro vyhledávání: '"Robert Behdadnia"'
Publikováno v:
Journal of Propulsion and Power. 26:1161-1170
*† ‡ § ** †† ‡‡ The occurrence of combustion oscillations has recently raised serious concerns about the development of scramjet engines. Previous studies on supersonic combustion for high-speed airbreathing propulsion applications indic
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::486731feb18fa9b247b2f1eae4f2fdc7
https://doi.org/10.2514/1.43338
https://doi.org/10.2514/1.43338
Publikováno v:
26th AIAA Applied Aerodynamics Conference.
In previous numerical simulations, a constant pressure boundary condition was imposed at the scramjet isolator exit to simulate the effect of the back-pressure valve in the experimental setup. This can, however, sometimes create a reverse flow near t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e85f95fb6fbe0585a41eaa8dffad78d2
https://doi.org/10.2514/6.2008-6929
https://doi.org/10.2514/6.2008-6929
Publikováno v:
43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1494e18effea7cdfff13ed3cfff1de1e
https://doi.org/10.2514/6.2007-5378
https://doi.org/10.2514/6.2007-5378
Autor:
Kevin Jackson, Fuhua Ma, Jian Li, Thomas A. Jackson, Robert Behdadnia, Vigor Yang, Kuo-Cheng Lin
Publikováno v:
43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4bf5c93c7f60f48586ac1d33cd57f9dc
https://doi.org/10.2514/6.2007-5382
https://doi.org/10.2514/6.2007-5382
Publikováno v:
42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::84be8743bf777abf697f1e4fe4f7128d
https://doi.org/10.2514/6.2006-4509
https://doi.org/10.2514/6.2006-4509
Publikováno v:
42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
A streamline-traced Busemann inlet was tested in the Virginia Tech supersonic blowdown wind tunnel in a Mach 4.08 freestream flow. These tests involved the starting and operational characteristics of a high contraction ratio (10) circular inlet, comm
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::81276edc17cae354cd58617ee2238881
https://doi.org/10.2514/6.2006-4508
https://doi.org/10.2514/6.2006-4508
Publikováno v:
AIAA/CIRA 13th International Space Planes and Hypersonics Systems and Technologies Conference.
Controlling shock-wave/turbulent-boundary-layer interactions is one of the most important roles of a scramjet isolator, particularly in the effort to prevent inlet unstart. Three-dimensional, steady-state numerical simulations were performed to impro
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1e821d384b570919928603adda559e9e
https://doi.org/10.2514/6.2005-3286
https://doi.org/10.2514/6.2005-3286