Effect of cavity location on combustion flow field of integrated hypersonic vehicle in near space
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概要
- 論文の詳細を見る
- 2011-12-01
著者
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LIU Jun
Center for Endemic Disease Control and Research of Inner Mongolia
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Wang Zhen
Center Of Hypersonic Propulsion College Of Aerospace And Materials Engineering National University O
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Huang Wei
Center Of Bme Beijing University Of Technology
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Jin Liang
Center Of Hypersonic Propulsion College Of Aerospace And Materials Engineering National University Of Defense Technology
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Huang Wei
Center Of Hypersonic Propulsion College Of Aerospace And Materials Engineering National University Of Defense Technology
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Liu Jun
Center Of Hypersonic Propulsion College Of Aerospace And Materials Engineering National University Of Defense Technology
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WANG Zhen
Center of Hypersonic Propulsion, College of Aerospace and Materials Engineering, National University of Defense Technology
関連論文
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- SIMULATION OF HEMODYNAMICS IN ABDOMINAL AORTA(Cardiovascular flow Simulation)
- Investigation on the flameholding mechanisms in supersonic flows : backward-facing step and cavity flameholder
- Effect of cavity location on combustion flow field of integrated hypersonic vehicle in near space