首页> 美国政府科技报告 >Space Shuttle technology preliminary data. Static stability characteristics of MSC Orbiter: Effect of Reynolds number and body corner radius at M less than or equal to 0.5

【24h】

Space Shuttle technology preliminary data. Static stability characteristics of MSC Orbiter: Effect of Reynolds number and body corner radius at M less than or equal to 0.5

机译：航天飞机技术初步数据。 msC Orbiter的静态稳定特性：雷诺数和体角半径在m小于或等于0.5时的影响

获取原文

页面导航

摘要
著录项
相似文献
相关主题

摘要

The effects of Reynolds number and body corner radius on the aerodynamic characteristics of a model of the proposed MSC Space Shuttle Orbiter have been investigated and the results are presented. The model, a modified May 1969 baseline shape, was tested in the Ames 12-Foot Pressure Wind Tunnel during November 1969.

著录项

作者

展开▼
作者单位

展开▼
年度 1970
页码 1-227
总页数 227
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
AERODYNAMIC CHARACTERISTICS; FLIGHT STABILITY TESTS; REYNOLDS NUMBER; SPACE SHUTTLE ORBITERS; SPACECRAFT MODELS; SPACECRAFT STABILITY; STATIC STABILITY; WIND TUNNEL MODELS; WIND TUNNEL TESTS; ANGLE OF ATTACK; SPACECRAFT CONFIGURATIONS;

机译：空气动力学特征;飞行稳定性测试; REYNOLDs NUmBER; spaCE sHUTTLE ORBITERs;航天器模型;航天器稳定性;静态稳定性;风洞模型;风洞隧道测试;攻击角度;航天器配置;

相似文献

外文文献
中文文献
专利

1. VARIATIONAL PROPERTIES AND LINEAR STABILITIES OF SPATIAL ISOSCELES ORBITS IN THE EQUAL-MASS THREE-BODY PROBLEM [J] . Tiancheng Ouyang, Duokui Yan Discrete and continuous dynamical systems . 2017,第7期

机译：等量三体问题中空间等距轨道的变化性质和线性稳定性
2. LINEAR STABILITY OF THE CRISS-CROSS ORBIT IN THE EQUAL-MASS THREE-BODY PROBLEM [J] . XIAOJUN CHANG, TIANCHENG OUYANG, DUOKUI YAN Discrete and continuous dynamical systems . 2016,第11期

机译：等质量三体问题中的交叉轨道的线性稳定性
3. INSTABILITY OF THE PERIODIC HIP-HOP ORBIT IN THE 2N-BODY PROBLEM WITH EQUAL MASSES [J] . Mark Lewis, Daniel Offin, PlETRO-LUCIANO BUONO, Discrete and continuous dynamical systems . 2013,第3期

机译：等质量的2N体问题中周期Hip-Hop轨道的不稳定性
4. ACOUSTIC TEST RESPONSE ANALYSIS OF THE SPACE SHUTTLE ORBITER BODY FLAP [C] . John S. Cheng, Michael Dunham, Jack Joanides International Modal Analysis Conference Exhibit . 2004

机译：空间梭子轨道机体皮瓣的声学试验响应分析
5. Influence of Reynolds number on flow and aerodynamic characteristics of bluff bodies with rectangular section of cut corners [O] . Atsushi OKAJIMA, Hisanori UENO, Akihito ABE 1991

机译：雷诺数对狭窄矩形矩形块状物流和空气动力学特性的影响
6. Effects of Reynolds number and body corner radius on aerodynamic characteristics of a space shuttle-type vehicle at subsonic Mach numbers [R] . Jorgensen, L. H., Brownson, J. J. 1972

机译：雷诺数和体角半径对亚音速马赫数下航天飞行器气动特性的影响

Space Shuttle technology preliminary data. Static stability characteristics of MSC Orbiter: Effect of Reynolds number and body corner radius at M less than or equal to 0.5

摘要

著录项

相似文献

相关主题

期刊订阅