首页> 美国政府科技报告 >Transonic investigation of the effectiveness and loading characteristics of a flap-type aileron with and without paddle balances of an unswept-wing-fuselage model

【24h】

Transonic investigation of the effectiveness and loading characteristics of a flap-type aileron with and without paddle balances of an unswept-wing-fuselage model

机译：具有和不具有平衡翼型机翼模型的襟翼式副翼的有效性和载荷特性的跨声速研究

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
Hieser, Gerald;
展开▼
作者单位

展开▼
年度 1956
页码 1-42
总页数 42
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词

相似文献

外文文献
中文文献
专利

1. Investigation of Outside Heat Balance Models for Use in a Heat Balance Cooling Load Calculation Procedure [J] . Todd M McClellan Curtis O Pedersen ASHRAE Transactions . 1997,第2期

机译：用于热平衡冷却负荷计算程序的外部热平衡模型的研究
2. Investigation of winglet on the transonic flutter characteristics for a wind tunnel test model CHNT-1 [J] . Lv Binbin, Lu Zhiliang, Guo Tongqing, Aerospace science and technology . 2019,第MARa期

机译：基于CHNT-1风洞试验模型的小翼对跨音速颤振特性的研究
3. Investigation of the Three-Dimensional Hinge Moment Characteristics Generated by the ONERA-M6 Wing with an Aileron [J] . G. Q. Zhang, S. C. M. Yu, A. Chien Advances in Mechanical Engineering . 2013,第Pta5期

机译：带有副翼的ONERA-M6机翼产生的三维铰链矩特性的研究
4. NUMERICAL INVESTIGATION OF AN AILERON HINGE MOMENTS AND EFFECTIVENESS ON A HIGH LIFT WING AIRFOIL [C] . K.A.Makarov, A.A.Pavlenko Congress of the International Council of the Aeronautical Sciences;International Council of the Aeronautical Sciences . 2014

机译：高升力机翼翼型铰链弯矩的数值研究及效果
5. Load balancing in hop-by-hop routing with and without traffic splitting. [D] . Wang, Jun. 2003

机译：逐跳路由中的负载均衡，带有和不带有流量分割。
6. Modulation of working memory load distinguishes individuals with and without balance impairments following mild traumatic brain injury [O] . Elizabeth J. Woytowicz, Chandler Sours, Rao P. Gullapalli, -1

机译：工作记忆负荷的调节可区分轻度脑外伤后有平衡障碍和无平衡障碍的个体
7. Wing And Fin Load Characteristics Of 1/15 Scale Lca Sge 26d Flow Through Model Tested At 8' X 8' Transonic Pd Ea 9211 Wind-Tunnel, Calspan U .S .A .udud [O] . Seshadri SN, Dutt HNV 1992

机译：1/15比例Lca Sge 26d流经模型的机翼和鳍载荷特性在美国Calspan美国8'X 8'Transonic Pd Ea 9211风洞测试 ud ud

Transonic investigation of the effectiveness and loading characteristics of a flap-type aileron with and without paddle balances of an unswept-wing-fuselage model

摘要

著录项

引文网络

相似文献

相关主题

期刊订阅