首页> 美国政府科技报告 >Investigation of support system effects on orbiter low speed aerodynamic characteristics using 0.0405-scale model (43-0) in the NAAL low speed wind tunnel (OA176)

【24h】

Investigation of support system effects on orbiter low speed aerodynamic characteristics using 0.0405-scale model (43-0) in the NAAL low speed wind tunnel (OA176)

机译：在NaaL低速风洞（Oa176）中使用0.0405比例模型（43-0）研究支持系统对轨道器低速气动特性的影响

获取原文

页面导航

摘要
著录项
引文网络
相似文献
相关主题

摘要

No Abstract Available

著录项

作者
Hughes, M. T.;
展开▼
作者单位

展开▼
年度 1980
页码 1-626
总页数 626
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
AERODYNAMIC CHARACTERISTICS; SPACE SHUTTLE ORBITERS; WIND TUNNEL TESTS; AEROTHERMODYNAMICS; LOW SPEED WIND TUNNELS; SCALE MODELS; SUBSONIC SPEED;

机译：空气动力学特征; spaCE sHUTTLE ORBITERs;风洞隧道测试;气动热力学;低速风洞;尺度模型; sUBsONIC spEED;

相似文献

外文文献
中文文献
专利

1. Supporting system interference on aerodynamic characteristics of an aircraft model in a low-speed wind tunnel [J] . Ocokoljic Goran, Rasuo Bosko, Kozic Mirko Aerospace science and technology . 2017,第MAY期

机译：支持系统对低速风洞中飞机模型空气动力特性的干扰
2. Model Aerodynamic Tests with a Wire-driven Parallel Suspension System in Low-speed Wind Tunnel [J] . Xiao Yangwen, Lin Qi, Zheng Yaqing, 中国航空学报（英文版） . 2010,第004期
3. Model Aerodynamic Tests with a Wire-driven Parallel Suspension System in Low-speed Wind Tunnel [J] . Xiao Yangwen, Lin Qi, Zheng Yaqing, 中国航空学报：英文版 . 2010,第004期

机译：在低速风洞中采用线驱动并联悬架系统进行空气动力学模型试验
4. MODELING AND CONTROL OF A WIRE-DRIVEN PARALLEL SUPPORT SYSTEM WITH LARGE ATTACK ANGLES IN LOW SPEED WIND TUNNELS [C] . Lin Qi, Zheng Ya-qing, Liu Xiong-wei Congress of the International Council of the Aeronautical Sciences . 2006

机译：低速风隧道大攻击角的电线驱动平行支撑系统的建模与控制
5. Initial investigations of transonic turbine aerodynamics using the Carleton University High-Speed Wind Tunnel. [D] . Jeffries, Michael Scott. 2001

机译：使用卡尔顿大学高速风洞进行跨音速涡轮空气动力学的初步研究。
6. Aerodynamic evaluation of wing shape and wing orientation in four butterfly species using numerical simulations and a low-speed wind tunnel and its implications for the design of flying micro-robots [O] . Alejandro Ortega Ancel, Rodney Eastwood, Daniel Vogt, 2017

机译：利用数值模拟和低速风洞对四种蝶类的翼形和翼向进行空气动力学评估及其对飞行微型机器人设计的启示
7. Model Aerodynamic Tests with a Wire-driven Parallel Suspension System in Low-speed Wind Tunnel [O] . 肖扬文, 林麒, 郑亚青, 2010

机译：在低速风洞中使用线驱动并联悬架系统进行空气动力学模型试验
8. SPACE SHUTTLE VEHICLE FERRY CONFIGURATION AFTERBODY FAIRING EFFECTS ON 140A/B ORBITER AERODYNAMIC CHARACTERISTICS USING AN 0405-SCALE MODEL ORBITER (43-0) IN THE ROCKWELL INTERNATIONAL 7.75 x 11 FT LOW SPEED WIND TUNNEL (0A123) [R] . R. C. Mennell 1975

机译：在洛克威尔国际7.75 x 11 FT低速风洞（0a123）中使用0405-sCaLE模型轨道（43-0）对空间穿梭车辆配置后140a / B轨道空气动力学特性

Investigation of support system effects on orbiter low speed aerodynamic characteristics using 0.0405-scale model (43-0) in the NAAL low speed wind tunnel (OA176)

摘要

著录项

引文网络

相似文献

相关主题

期刊订阅