Zobrazeno 1 - 10
of 47
pro vyhledávání: '"Chung-Jen Tam"'
Publikováno v:
Proceedings of the Combustion Institute. 35:2101-2108
Ignition of an ethylene fueled cavity in a supersonic flow was achieved through the application of two energy deposition techniques: a spark discharge and pulse detonator ( PD ). High-frequency shadowgraph and chemiluminescence imaging showed that th
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2b46a3d389052fe831b5af1f36cecd31
https://doi.org/10.1016/j.proci.2014.07.068
https://doi.org/10.1016/j.proci.2014.07.068
Publikováno v:
54th AIAA Aerospace Sciences Meeting.
This research effort addresses the use of numerical simulations to predict the flow physics over an airborne turret, represented by a hemisphere. Computational fluid dynamics codes, Loci-Chem, Kestrel and OVERFLOW were used in this study with differe
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::17e4d2882167564af710a92ac63806ca
https://doi.org/10.2514/6.2016-1458
https://doi.org/10.2514/6.2016-1458
Publikováno v:
AIAA Journal. 47:2379-2390
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e4500efe02f789ba6d5a715ceeefbbb5
https://doi.org/10.2514/1.41077
https://doi.org/10.2514/1.41077
Autor:
Chung-Jen Tam, Kevin Jackson, Ryan N. Givens, William F. Bailey, William F. Terry, Skip Williams, Chadwick D. Lindstrom
Publikováno v:
AIAA Journal. 47:2368-2378
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e9b22ebc45940a0b1133f8fef2fbce98
https://doi.org/10.2514/1.41074
https://doi.org/10.2514/1.41074
Autor:
Campbell D. Carter, Spencer Kuo, Thomas A. Jackson, Jack Barnett, Daniel Bivolaru, Skip Williams, Robert A. Baurle, Lance S. Jacobsen, Chung-Jen Tam
Publikováno v:
Journal of Propulsion and Power. 24:641-654
This study assesses the prospect of main-fuel ignition with plasma-generating devices in a supersonic flow. Progress from this study has established baseline conditions for operation, such as the required operational time of a device to initiate a co
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7c712e5f0e11ec907de9e865a3fe507c
https://doi.org/10.2514/1.27358
https://doi.org/10.2514/1.27358
Publikováno v:
46th AIAA Plasmadynamics and Lasers Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::724a6d143d6f67847887580e31f0c57d
https://doi.org/10.2514/6.2015-2503
https://doi.org/10.2514/6.2015-2503
Publikováno v:
Notes on Numerical Fluid Mechanics and Multidisciplinary Design ISBN: 9783319119663
Enhanced mixing and conditioning of a transverse jet in Mach-2 cross flow was investigated through the application of a staged pulse detonation injector. NO planar laser-induced fluorescence and high-frame-rate shadowgraph imaging provided measuremen
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a5ef32f80fc0ea488248a1f6c11bd9ce
https://doi.org/10.1007/978-3-319-11967-0_16
https://doi.org/10.1007/978-3-319-11967-0_16
Publikováno v:
52nd Aerospace Sciences Meeting.
Ignition of an ethylene fueled cavity in a supersonic flow was achieved through the application of two energy deposition techniques: a spark discharge and pulse detonator (PD). High-frequency shadowgraph and chemiluminescence imaging showed that the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::32dafe4d71939f2aceeadec4d04c8112
https://doi.org/10.2514/6.2014-0286
https://doi.org/10.2514/6.2014-0286
Publikováno v:
AIAA Journal. 34:2255-2260
A time-accurate double thin-layer Navier-Stokes computation is performed for an unsteady supersonic open cavity with a length-to-depth ratio of 2. The results are used to determine the flow-physics mechanisms responsible for the cavity oscillation cy
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::30062fba258f4f80c375dac37d0b91e8
https://doi.org/10.2514/3.13388
https://doi.org/10.2514/3.13388
Publikováno v:
30th AIAA Applied Aerodynamics Conference.
Direct-connect wind-tunnel facilities that produce uniform flow entering the test section are generally used for scramjet-component (isolator/combustor) studies. In freejet experiments and flight tests, however, air enters the engine through an inlet
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::a67419681e6387be6ee614b65a5a0237
https://doi.org/10.2514/6.2012-3224
https://doi.org/10.2514/6.2012-3224