首页> 美国政府科技报告 >Airloads investigation of an 0.030-scale model of the Space Shuttle Vehicle 140 A/B launch configuration (model 47-OTS) in the ARC 11-foot Unitary Plan Wind Tunnel for MACH range 0.6 to 1.4 (IA14A), volume 10

【24h】

Airloads investigation of an 0.030-scale model of the Space Shuttle Vehicle 140 A/B launch configuration (model 47-OTS) in the ARC 11-foot Unitary Plan Wind Tunnel for MACH range 0.6 to 1.4 (IA14A), volume 10

机译：airloads调查了一架0.030比例的航天飞机车辆140 a / B发射配置（型号47-OTs），用于aRC 11英尺单一平面风洞，适用于maCH 0.6至1.4（Ia14a），第10卷

获取原文

页面导航

摘要
著录项
相似文献
相关主题

摘要

Pressure data are presented in tabular form on the external tank base and SRM booster base of the space shuttle launch vehicle configuration model. For Vol. 3, see N75-23657.

著录项

作者
Gillins, R. L.;
展开▼
作者单位

展开▼
年度 1975
页码 1-853
总页数 853
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
AERODYNAMIC LOADS; LAUNCH VEHICLE CONFIGURATIONS; SPACE SHUTTLE ASCENT STAGE; SPACE SHUTTLES; WIND TUNNEL TESTS; AERODYNAMIC STABILITY; ANGLE OF ATTACK; EXTERNAL TANKS; MACH NUMBER; SPACE SHUTTLE BOOSTERS; SUBSONIC SPEED; SUPERSONIC SPEED; TRANSONIC SPEED; WIND TUNNELS;

机译：空气动力负荷;发射车辆配置;空间穿梭阶段;太空沙滩;风洞隧道测试;空气动力学稳定性;攻击角度;外部坦克;马赫数; spaCE sHUTTLE BOOsTERs; sUBsONIC spEED;超音速;跨音速;风洞;

相似文献

外文文献
专利

1. A Preliminary Investigation of the Check Standard Model in the NASA Ames Unitary Plan Wind Tunnel [C] . Max Amaya, Ross Flach, Theodore J. Garbeff Ⅱ AIAA aviation forum . 2019

机译：NASA Ames单一计划风洞中检查标准模型的初步研究

Airloads investigation of an 0.030-scale model of the Space Shuttle Vehicle 140 A/B launch configuration (model 47-OTS) in the ARC 11-foot Unitary Plan Wind Tunnel for MACH range 0.6 to 1.4 (IA14A), volume 10

摘要

著录项

相似文献

相关主题

期刊订阅