首页> 美国政府科技报告 >WIND-TUNNEL INVESTIGATION AT MACH NUMBERS FROM 0.40 TO 1.20 OF THE STATIC AERODYNAMIC AND CONTROL CHARACTERISTICS OF A MODEL OF A NONLIFTING REENTRY CAPSULE IN COMBINATION WITH A ROCKET BOOSTER

【24h】

WIND-TUNNEL INVESTIGATION AT MACH NUMBERS FROM 0.40 TO 1.20 OF THE STATIC AERODYNAMIC AND CONTROL CHARACTERISTICS OF A MODEL OF A NONLIFTING REENTRY CAPSULE IN COMBINATION WITH A ROCKET BOOSTER

机译：静力空气动力学0.40~1.20的机械数值研究及与火箭推进器结合的非提升式再生胶囊模型的控制特性

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

Wind tunnel investigation at subsonic & transonic speed of static aerodynamic and control characteristics of capsule-booster model

著录项

作者
Pearson, A. O.;
展开▼
作者单位

展开▼
年度 1960
页码 1-69
总页数 69
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
BOOSTER ROCKET ENGINES; CAPSULES; CONTROL; MACH NUMBER; REENTRY VEHICLES; REYNOLDS NUMBER; STATIC AERODYNAMIC CHARACTERISTICS; SUBSONIC SPEED; TRANSONIC SPEED; WIND TUNNELS; BOOSTER; CAPSULE; CONTROL; REENTRY VEHICLE; STATIC AERODYNAMIC CHARACTERISTICS; SUBSONIC SPEED; TRANSONIC SPEED; WIND TUNNEL;

机译：BOOsTER ROCKET ENGINEs;胶囊;控制;马赫数; REENTRY车辆; REYNOLDs NUmBER;静态空气动力学特性; sUBsONIC spEED;跨音速;风洞; BOOsTER;胶囊;控制; REENTRY VEHICLE;静态空气动力学特性; sUBsONIC spEED;跨音速;风洞;

相似文献

外文文献
中文文献
专利

1. Evaluating Aerodynamic Characteristics of Wind-Tunnel Models Produced by Rapid Prototyping Methods [J] . A. Springer Journal of Spacecraft and Rockets . 1998,第6期

机译：快速原型方法产生的风洞模型的空气动力学特性评估
2. Modeling of reentry space vehicle aerodynamics with control thruster plume - free-stream interaction [J] . Kashkovsky A. V., Vashchenkov P. V., Banyai T. Thermophysics and Aeromechanics . 2014,第6期

机译：带有可控推进器羽-自由流相互作用的再入航天器空气动力学建模。
3. 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
4. Aerodynamic Characterization and Simulation of a Solid Rocket Booster During Reentry Flight [C] . David C. Purinton, John A. Blevins, Victor Pritchett, AIAA aerospace sciences meeting including the new horizons forum and aerospace exposition . 2011

机译：再入飞行中固体火箭助推器的气动特性与仿真
5. Aerodynamic Characteristics of a Feathered Dinosaur Measured Using Physical Models. Effects of Form on Static Stability and Control Effectiveness [O] . Dennis Evangelista, Griselda Cardona, Eric Guenther-Gleason, -1

机译：使用物理模型测量的羽毛恐龙的空气动力学特性。形式对静态稳定性和控制有效性的影响
6. Simple Aerodynamic Modeling for Estimating Static Aeroelastic Deformation of Wind-Tunnel Models [O] . Yoshikazu MAKINO, Keisuke OHIRA, Takuya MAKIMOTO, 2011

机译：估算风洞模型静态空气弹性变形的简单空气动力学建模

WIND-TUNNEL INVESTIGATION AT MACH NUMBERS FROM 0.40 TO 1.20 OF THE STATIC AERODYNAMIC AND CONTROL CHARACTERISTICS OF A MODEL OF A NONLIFTING REENTRY CAPSULE IN COMBINATION WITH A ROCKET BOOSTER

摘要

著录项

引文网络

相似文献

相关主题

期刊订阅