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Three- Dimensional Flowfield in the Scaled Payload/Fairing Model of an Expendable Launch Vehicle

机译：消耗性运载火箭的成比例有效载荷/公平模型中的三维流场

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《AIAA Fluid Dynamics Conference and Exhibit》|2008年|P.1-21|共21页
会议地点 Seattle WA(US)
作者
R. Nallasamy; M. Kandula; L. Duncil; P. Schallhorn;
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作者单位

ASRC Kennedy Space Center FL;

NASA Kennedy Space Center FL;

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2. Response Surface Equations for Expendable Launch Vehicle Payload Mass Capability [J] . Jarret M. Lafleur, Elizabeth S. Fleming, Joseph H. Saleh Journal of Spacecraft and Rockets . 2012,第1期

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4. Three- Dimensional Flowfield in the Scaled Payload/Fairing Model of an Expendable Launch Vehicle [C] . American Institute of Aeronautics and Astronautics Fluid Dynamics Conference and Exhibit . 2008

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6. Modeling Vehicle Collision Angle in Traffic Crashes Based on Three-Dimensional Laser Scanning Data [O] . Nengchao Lyu, Gang Huang, Chaozhong Wu, 2017

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7. Initial Structural-Acoustic Modeling and Control Results for a Full-Scale Composite Payload Fairing for Acoustic Launch Load Alleviation [O] . Roger M. Glaese, Eric H. Anderson 2016

机译：用于声发射负荷缓解的全尺寸复合有效载荷整流的初始结构 - 声学建模和控制结果
8. Initial Structural-Acoustic Modeling and Control Results for a Full- Scale Composite Payload Fairing for Acoustic Launch Load Alleviation [R] . Glaese, R. M. , Anderson, E. H. 1999

机译：用于声发射负荷缓解的全尺寸复合有效载荷整流的初始结构 - 声学建模和控制结果

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