首页> 美国政府科技报告 >Space shuttle: IRLV straight wing orbiter (model 130c) longitudinal and lateral static stability characteristics during configuration build-up; horizontal tail control effectiveness. Wind tunnel test results

【24h】

Space shuttle: IRLV straight wing orbiter (model 130c) longitudinal and lateral static stability characteristics during configuration build-up; horizontal tail control effectiveness. Wind tunnel test results

机译：航天飞机：IRLV直翼航天飞机（型号130c）在配置建立期间的纵向和横向静态稳定特性;水平尾部控制效果。风洞试验结果

获取原文

页面导航

摘要
著录项
相似文献
相关主题

摘要

Low speed longitudinal, directional, and lateral static stability characteristics of straight wing orbiter during configuration build-up

著录项

作者
Mennell, R.;
展开▼
作者单位

展开▼
年度 1970
页码 1-275
总页数 275
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
AERODYNAMIC CONFIGURATIONS; LATERAL STABILITY; LONGITUDINAL STABILITY; AERODYNAMIC CHARACTERISTICS; ANGLE OF ATTACK; LOW SPEED WIND TUNNELS;

机译：空气动力学配置;横向稳定性;纵向稳定性;空气动力学特征;攻击角度;低速风洞;

相似文献

外文文献
专利

1. Joined-Wing Wind-Tunnel Test for Longitudinal Control via Aftwing Twist [J] . Vanessa L. Bond Journal of Aircraft . 2010,第5期

机译：通过机翼扭转进行纵向控制的联合翼风洞试验
2. Joined-Wing Wind-Tunnel Test for Longitudinal Control via Aftwing Twist [J] . Vanessa L. Bond, rnRobert A. Canfield, rnMaria da Luz Madruga Santos Matos, Journal of Aircraft . 2010,第5期

机译：通过机翼扭转进行纵向控制的联合翼风洞试验
3. Active Aeroelastic Control Over a Multisurface Wing: Modeling and Wind-Tunnel Testing [J] . A. De Gaspari, S. Ricci, L. Riccobene, AIAA Journal . 2009,第9期

机译：多翼机翼的主动气动弹性控制：建模和风洞测试
4. On Problems Associated with Modeling Wing- Tail Configurations from Wind Tunnel Data [C] . P. Murphy, V. Klein AIAA Guidance, Navigation and Control Conference and Exhibit; AIAA Atmospheric Flight Mechanics Conference and Exhibit; AIAA Modeling and Simulation Technologies Conference and Exhibit . 2007

机译：基于风洞数据的机翼尾翼建模相关问题
5. Wind tunnel tests on the effect of power on the stability of a low wing monoplane with three vertical positions of horizontal tail surfaces [O] . Bolster Calvin Mathews 1936

机译：风洞试验功率对水平尾翼三个垂直位置的低翼单翼飞机稳定性的影响

Space shuttle: IRLV straight wing orbiter (model 130c) longitudinal and lateral static stability characteristics during configuration build-up; horizontal tail control effectiveness. Wind tunnel test results

摘要

著录项

相似文献

相关主题

期刊订阅