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Results of an investigation of the space shuttle solid rocket booster aerodynamic heating characteristics obtained using the 0.0175-scale model 60-OTS in AEDC tunnel A during tests IH47, volume 2

机译：在IH47，第2卷的测试中，使用0.0175比例模型60-OTs在aEDC隧道a中获得的航天飞机固体火箭助推器气动加热特性的研究结果

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作者
Dye, W. H.;
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年度 1977
页码 1-803
总页数 803
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
AERODYNAMIC HEATING; ROCKET TEST FACILITIES; SCALE MODELS; SPACE SHUTTLE BOOSTERS; WIND TUNNEL TESTS; SPACECRAFT CONFIGURATIONS; SPACECRAFT MODELS; TABLES (DATA); THERMOCOUPLES;

机译：空气动力加热;火箭测试设施;尺度模型; spaCE sHUTTLE BOOsTERs;风洞隧道测试;航天器配置;航天器模型;表（数据）;热电偶;

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1. Wind Tunnel Experimental Investigation on the Aerodynamic Characteristics of the Multifin Rockets and Missiles [J] . HAO Lu, WU Jia-sheng Journal of Beijing Institute of Technology . 2005,第3期

机译：多翅火箭弹气动特性的风洞实验研究
2. Simulated Models Test Design of Space Shuttles and Rocket Engines [J] . NASA Tech Briefs . 2008,第5期

机译：航天飞机和火箭发动机的仿真模型测试设计
3. Numerical simulation of the side pylon effect on the aerodynamic characteristics of models at their wind tunnel tests [J] . Volkov V. F., Mazhul I. I., Zvegintsev V. I. Thermophysics and Aeromechanics . 2016,第3期

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4. Ice Impact Testing on the Space Shuttle Solid Rocket Boosters [C] . H. Kanner, K. Hamlin AIAA Aerospace Sciences Meeting and Exhibit . 2006

机译：航天飞机固体火箭助推器的冰撞击测试
5. AN INVESTIGATION OF THE THEORETICAL AND EXPERIMENTAL AERODYNAMIC CHARACTERISTICS OF A LOW-CORRECTION WIND TUNNEL WALL CONFIGURATION FOR AIRFOIL TESTING. [D] . MALEK, AHMED FOUAD HASSAN. 1983

机译：用于翼型测试的低校正风洞墙构型的理论和实验气动特性研究。
6. Recession Curve Generation for the Space Shuttle Solid Rocket Booster Thermal Protection System Coatings [O] . Kanner Howard S., Davis Darrell, Davis Darrell W., 2002

机译：航天飞机固体火箭助推器热防护系统涂层的衰退曲线生成
7. Results of an investigation of the space shuttle integrated vehicle aerodynamic heating characteristics obtained using the 0.0175-scale model 60-OTS in AEDC tunnel A during tests IH41B, volume 1 [R] . Dye, W. H. 1977

机译：在测试IH41B，第1卷中使用0.0175比例模型60-OTs在aEDC隧道a中获得的航天飞机综合车辆空气动力学加热特性的调查结果

Results of an investigation of the space shuttle solid rocket booster aerodynamic heating characteristics obtained using the 0.0175-scale model 60-OTS in AEDC tunnel A during tests IH47, volume 2

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