Zobrazeno 1 - 10
of 27
pro vyhledávání: '"Dean Eklund"'
Autor:
Ez A. Hassan, Mark A. Hagenmaier, D. Keith Walters, Edward A. Luke, David M. Peterson, Dean Eklund
Publikováno v:
Flow, Turbulence and Combustion. 99:437-459
Simulations of an experimental hydrogen-fueled scramjet combustor are conducted using a novel dynamic hybrid Reynolds-averaged Navier-Stokes/large-eddy simulation (DHRL) modeling framework. The combustor has a Mach 2 core flow with a ramp fuel inject
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::53d7d1b5c680b408424a3d49be0d7075
https://doi.org/10.1007/s10494-017-9821-2
https://doi.org/10.1007/s10494-017-9821-2
Publikováno v:
AIAA Journal. 53:1405-1423
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::99325a00327cfc666460adae88b0a0d0
https://doi.org/10.2514/1.j053280
https://doi.org/10.2514/1.j053280
Publikováno v:
Journal of Propulsion and Power. 27:1317-1320
A PRELIMINARY numerical characterization of a U.S. Air Force Research Laboratory (AFRL) test facility was performed. Research cell 22 (RC22) is a supersonic wind-tunnel facility at AFRL. RC22 is presently simulating dual-mode combustion for circular
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::667645bf99800746231a7b1ba8a98d13
https://doi.org/10.2514/1.b34178
https://doi.org/10.2514/1.b34178
Publikováno v:
53rd AIAA Aerospace Sciences Meeting.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::732ba631a7e7a941b01f8716cc3ac49e
https://doi.org/10.2514/6.2015-0502
https://doi.org/10.2514/6.2015-0502
Publikováno v:
50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference.
A numerical framework is presented for CFD-based uncertainty quantification (UQ) involving propagation of combined aleatory and epistemic uncertainties to relevant output quantities, with intended application to scramjet inlet analysis. Latin hypercu
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e32271f09026f440ef564cab47f010b5
https://doi.org/10.2514/6.2014-3844
https://doi.org/10.2514/6.2014-3844
Publikováno v:
52nd Aerospace Sciences Meeting.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::664c331ab5ff5a1d564efd3a87372676
https://doi.org/10.2514/6.2014-0576
https://doi.org/10.2514/6.2014-0576
Autor:
Dean Eklund, Mark R. Gruber, Charles Smith, Jeffrey M. Donbar, Tarun Mathur, Robert A. Baurle, Kevin Jackson
Publikováno v:
Journal of Propulsion and Power. 17:1296-1304
Anew continuous-e ow,direct-connect,high-enthalpy, supersonic combustion researchfacility isdescribed. This test facility provides combustor inlet e ow conditions corresponding to e ight Mach numbers between 3.5 and 7, at dynamic pressures up to 95.8
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::dd268e216269879649b9008089cfd10e
https://doi.org/10.2514/2.5878
https://doi.org/10.2514/2.5878
Autor:
Daniel Risha, Tarun Mathur, Chung-Jen Tam, Mark R. Gruber, Douglas Davis, Ryan T. Milligan, Jiwen Liu, Dean Eklund, Mark A. Hagenmaier
Publikováno v:
50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition.
Experiments were performed at the Air Force Research Laboratory's Propulsion Directorate (AFRL/RZ) in Research Cell 22 (RC22). Twelve cases from the experiment were computationally analyzed and each case varied in either engine operating condition an
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9d17c6b6ca7d5c5f6f1a78458f574db5
https://doi.org/10.2514/6.2012-947
https://doi.org/10.2514/6.2012-947
A technique to develop flight-like inflow conditions for direct-connect testing has been extended in the current work. This technique utilizes an expansion/contraction section upstream of the engine isolator in a direct-connect test facility to creat
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0bee580ec094f76e349580e205ef2ad0
https://doi.org/10.21236/ada543745
https://doi.org/10.21236/ada543745
Publikováno v:
49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition.
A technique to develop flight-like inflow conditions for direct-connect testing has been extended in the current work. This technique utilizes an expansion/contraction section upstream of the engine isolator in a direct-connect test facility to creat
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::fd0c15a86eca9385886cb624f31a2fc9
https://doi.org/10.2514/6.2011-233
https://doi.org/10.2514/6.2011-233