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Aerothermodynamic Analysis of the EXPERT Winglet: from the in- flight environment characterization to the rebuilding of the Scirocco Plasma Wind Tunnel test

机译：EXPERT小翼的空气热力学分析：从飞行中的环境表征到Scirocco等离子风洞测试的重建

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《16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference》|2009年|1-16|共16页
会议地点 Bremen(DE)
作者
S. Di;
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作者单位

Benedetto, M. Marini, G. Rufolo and R. Gardi, Centro Italiano Ricerche Aerospaziali (CIRA), Capua, Italy;

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原文格式 PDF
正文语种 eng
中图分类各类型航空器;
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专利

1. European Experimental Reentry Testbed Winglet: From In-Flight Characterization to SCIROCCO Test [J] . Sara Di Benedetto, Giuseppe C. Rufolo, Marco Marini, AIAA Journal . 2012,第10期

机译：欧洲实验性再入式试验台小翼：从飞行中表征到SCIROCCO测试
2. Experimental characterisation of the CIRA plasma wind tunnel SCIROCCO test section [J] . C. Purpura, F. De Filippis, P. Barrera, Acta astronautica . 2008,第6a7期

机译：CIRA等离子风洞SCIROCCO测试部分的实验表征
3. Performance Evaluation of Nose Cap to Silica Tile Joint of RLV-TD under the Simulated Flight Environment using Plasma Wind Tunnel Facility [J] . Aravindakshan Pillai, K. Krishnaraj, N. Sreenivas, Journal of The institution of engineers (India), Series C . 2017,第6期

机译：采用等离子风隧道设施下模拟飞行环境下RLV-TD鼻帽的性能评价
4. Aerothermodynamic Analysis of the EXPERT Winglet: from the in- flight environment characterization to the rebuilding of the Scirocco Plasma Wind Tunnel test [C] . S. Di American Institute of Aeronautics and Astronautics/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference . 2009

机译：专家翼面的空气运动分析：从飞行中的环境表征到柯卡科等离子隧道试验的重建
5. Design and Construction of a Wind Tunnel Model with Active Variable Camber Continuous Trailing Edge Flap for Aeroelastic 'In-flight' Shape Optimization Tests [D] . Precup, Nathan 2018

机译：主动可变弯度连续后缘襟翼风洞模型的设计与构建，用于气动弹性“飞行中”形状优化测试
6. Wind tunnel data of the analysis of heat pipe and wind catcher technology for the built environment [O] . John Kaiser Calautit, Hassam Nasarullah Chaudhry, Ben Richard Hughes 2015

机译：建筑环境热管和集热器技术分析中的风洞数据
7. Estimation of Aerodynamic Characteristics from Flight Test Data. (2nd Report) Analysis Methods under In-Flight Wind Tunnel Test Concept. [O] . Osamu KOBAYASHI 1992

机译：飞行试验数据估计空气动力学特征。（第2次报告）在飞行中风洞试验概念下的分析方法。
8. Correlation of Full-Scale Drag Predictions with Flight Measurements on the C-141A Aircraft : Phase 2: Wind Tunnel Tests, Analysis, and Prediction Techniques. Volume 2: Wind Tunnel Test and Basic Data [R] . Macwilkinson, D. G., Blackerby, W. T., Paterson, J. H. 1974

机译：C-141a飞机上全尺寸阻力预测与飞行测量的相关性：第2阶段：风洞试验，分析和预测技术。第2卷：风洞试验和基本数据

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