Aerodynamic Heating Characteristics Over a Protuberance in Hypersonic Flows Using Fast Response Thermo Gauges
نویسندگان
چکیده
منابع مشابه
Parallel Computation in Hypersonic Aerodynamic Heating Problem
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ژورنال
عنوان ژورنال: International Journal of Aeronautical and Space Sciences
سال: 2010
ISSN: 2093-274X
DOI: 10.5139/ijass.2010.11.3.193