Mach 4 Simulation Tests on Combustion and Unstart Processes of a Scramjet Engine. Observation of Internal Flow Structure.
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چکیده
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effect of sub-grid scales on large eddy simulation of particle deposition in a turbulent channel flow
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15 صفحه اولScramjet Combustion Processes
Research into hypersonic flow phenomona has been conducted by numerous groups within Australia for over 40 years. The genesis of all the modern day work can be traced back to the return of the then Dr Ray Stalker from England, to take a faculty position in the Physics Department of the Australian National University, Canberra, in 1962. Dr Stalker had a keen interest in the aerodynamics of bodie...
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ژورنال
عنوان ژورنال: JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
سال: 2001
ISSN: 1344-6460
DOI: 10.2322/jjsass.49.400