Zobrazeno 1 - 8
of 8
pro vyhledávání: '"M. S. Balasubramanyam"'
Publikováno v:
International Journal of Hypersonics. 1:181-198
Tests were performed in a non-axisymmetric, single nozzle, strut-based ejector to investigate mass flow entrainment, choking mechanisms and stream mixing as a function of primary (strut nozzle) to secondary (duct inlet) flow stagnation pressure ratio
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a777d844844d8c0103b8dc2a6c3e96aa
https://doi.org/10.1260/1759-3107.1.3.181
https://doi.org/10.1260/1759-3107.1.3.181
Publikováno v:
Engineering Applications of Computational Fluid Mechanics. 4:314-325
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::cc72fe9dfcb8adeca8fb2d1c2a202907
https://doi.org/10.1080/19942060.2010.11015319
https://doi.org/10.1080/19942060.2010.11015319
Autor:
C. P. Chen, M. S. Balasubramanyam
Publikováno v:
International Journal of Heat and Mass Transfer. 51:3896-3905
Numerical study of liquid atomization/spray process in a high speed cross-flow is described in this paper. Due to the strong aero-thermal dynamics/spray interaction, droplet evaporation process plays an important role even for non-chemical reacting c
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::90ed40ecfd0c7cecc4c00aac8c2fd6e6
https://doi.org/10.1016/j.ijheatmasstransfer.2007.11.054
https://doi.org/10.1016/j.ijheatmasstransfer.2007.11.054
Publikováno v:
Journal of Heat Transfer. 129:1082-1086
A new approach to account for finite thermal conductivity and turbulence effects within atomizing droplets of an evaporating spray is presented in this paper. The model is an extension of the T-blob and T-TAB atomization/spray model of Trinh and Chen
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7c83415e32f6983526586adcc8f73b5f
https://doi.org/10.1115/1.2737481
https://doi.org/10.1115/1.2737481
Autor:
David M. Lineberry, Marlow D. Moser, Robert L. Ikard, M. S. Balasubramanyam, Robert A. Frederick
Publikováno v:
46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::07f2dc27f01bfe555756297f2904ffc1
https://doi.org/10.2514/6.2010-6737
https://doi.org/10.2514/6.2010-6737
Publikováno v:
Multiphase.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b02241177f5cf2ff35b63a7d232bdb44
https://doi.org/10.1615/ihtc13.p12.260
https://doi.org/10.1615/ihtc13.p12.260
Autor:
M. S. Balasubramanyam, C. P. Chen
Publikováno v:
41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
Rocket Based Combined Cycle (RBCC) engines operate within a wide range of Mach numbers and altitudes. Fundamental fluid dynamic mechanisms involve complex choking, mass entrainment, stream mixing and wall interactions. The Propulsion Research Center
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1394774673bf18cbcf9621ef2adb5409
https://doi.org/10.2514/6.2005-3712
https://doi.org/10.2514/6.2005-3712
Publikováno v:
41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
This paper describes numerical implementation and validation of a newly developed hybrid model, T-blob/T-TAB, into an existing computational fluid dynamics (CFD) program for primary and secondary breakup simulation of liquid jet atomization. This mod
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::bd38aa702f67250726d696df92239df6
https://doi.org/10.2514/6.2005-3973
https://doi.org/10.2514/6.2005-3973