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Aeroengine full state modeling technology
Author: ZhangJian
Tutor: HuangJinQuan
School: Nanjing University of Aeronautics and Astronautics
Course: Aeronautical and Astronautical Science and Technology
Keywords: Turbofan engine Component -level model Start Modeling Vectoring nozzle Adjustable guide vane angle
CLC: V231
Type: Master's thesis
Year: 2009
Downloads: 295
Quote: 1
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Abstract
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CLC: > Aviation, aerospace > Aviation > Aero-engine ( propulsion system ) > Engine theory
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