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Risk Mitigation Study for Instrumentation Layout Along Wing Leading Edge of 1.8 Scale Space Shuttle Model Using TSP

机译：用TSP沿着翼翼前沿的仪器仪表布局仪器缓解研究

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《American Institute of Aeronautics and Astronautics Aerospace Sciences Meeting and Exhibit》|2005年||共33页
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1. Dynamic Impact Tolerance of Space Shuttle Orbiter Wing Leading-Edge Panels [J] . Edwin L. Fasanella, Karen E. Jackson, Karen H. Lyle, Journal of Spacecraft and Rockets . 2008,第5期

机译：航天飞机轨道机翼前缘板的动态冲击容忍度
2. Simulation of orbital debris impact on the Space Shuttle wing leading edge [J] . Eric P. Fahrenthold, Roque J. Hernandez International journal of impact engineering . 2006,第1a12期

机译：轨道碎片撞击航天飞机机翼前缘的模拟
3. Flexible Plug Repair for Shuttle Wing Leading Edge [J] . NASA Tech Briefs . 2012,第2期

机译：航天飞机机翼前缘的灵活插头维修
4. Risk Mitigation Study for Instrumentation Layout Along Wing Leading Edge of 1.8 Scale Space Shuttle Model Using TSP [C] . G. Smolinski, M. Holden, J. Hubner AIAA Aerospace Sciences Meeting and Exhibit . 2005

机译：使用TSP的1.8％比例航天飞机模型的机翼前缘仪表布局的风险缓解研究
5. Flow visualization and three-dimensional characteristics of the leading edge vortex on a hovering model hummingbird wing. [D] . Swanton, Erik William M. 2008

机译：悬停模型蜂鸟机翼上的流动可视化和前缘涡旋的三维特征。
6. Multi-Scale Clustering of Lyme Disease Risk at the Expanding Leading Edge of the Range of Ixodes scapularis in Canada [O] . Marion Ripoche, Leslie Robbin Lindsay, Antoinette Ludwig, 2018

机译：在加拿大肩x骨范围扩大的前沿上莱姆病风险的多尺度聚类
7. Space Shuttle Orbiter Wing-Leading-Edge Panel Thermo-Mechanical Analysis for Entry Conditions [O] . Knight, Norman F., Jr., Raju, Ivatury S., Song, Kyongchan 2010

机译：进入条件的航天飞机轨道飞行器翼前缘板热力学分析
8. Free-spinning-tunnel investigation to determine the effect on spins and recoveries of wing leading-edge chord-extensions and drooped leading-edge flaps on scale models of two sweptback-wing fighter airplanes [R] . Wilson, Jack H, Klinar, Walter J 1953

机译：自由旋转隧道调查，以确定两个后掠翼战斗机飞机的比例模型对机翼前缘弦杆延伸和下垂前缘襟翼的旋转和恢复的影响

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