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Scramjet engine fuel supply system solutions research

Author: ZhangHua
Tutor: ShenChiBing
School: National University of Defense Science and Technology
Course: Aeronautical and Astronautical Science and Technology
Keywords: Scramjet Fuel supply system Design Static characteristics Dynamic characteristics Starting process
CLC: V235
Type: Master's thesis
Year: 2011
Downloads: 65
Quote: 0
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Abstract


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CLC: > Aviation, aerospace > Aviation > Aero-engine ( propulsion system ) > Air jet engine
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