首页> 外文OA文献 >Aeroelastic testing of LCA wing models - Model fabrication - Ground testing - Wind tunnel testing and Data analysisud

【2h】

Aeroelastic testing of LCA wing models - Model fabrication - Ground testing - Wind tunnel testing and Data analysisud

机译：LCA机翼模型的空气弹性测试-模型制作-地面测试-风洞测试和数据分析 ud

页面导航

摘要
著录项
相似文献
相关主题

摘要

Aeroelastic Testing Programme of Scaled Aeroelastic model of LCA half wing with rigid fuselage.

机译：带有刚性机身的LCA半机翼按比例缩放的气动弹性模型的气动弹性测试程序。

著录项

作者
Somashekar BR; Rama Murthy MR; Rajagopal P; Sundararajan D; Shashikala Rajappa; Annamma Samuel -; Janardhanam S;
展开▼
作者单位

展开▼
年度 1997
总页数
原文格式 PDF
正文语种 {"code":"en","name":"English","id":9}
中图分类

相似文献

外文文献
中文文献
专利

1. 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
2. Design and Testing of a Blended Wing Body Aeroelastic Wind-Tunnel Model [J] . Martin Carlsson, Jakob Kuttenkeuler Journal of Aircraft . 2003,第1期

机译：混合翼体气动弹性风洞模型的设计与测试
3. Design of aeroelasticity bench test for NACA0012 wing model in the low speed wind tunnel: Influence of wing's parameters on flutter speed [J] . Thi Tuyet Nhung Le, Chi-Cong Nguyen, Hoang Nam Vang International Journal of Mechanical Engineering and Applications . 2015,第1a3期

机译：低速风洞中NACA0012机翼模型的空气弹性台架试验设计：机翼参数对扑扑速度的影响
4. Active Aeroelastic Control over a Multi- Surface Wing: Modelling and Wind Tunnel Testing [C] . A. De AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference . 2007

机译：多表面机翼的主动气动弹性控制：建模和风洞测试
5. Design and Construction of a Wind Tunnel Model with Active Variable Camber Continuous Trailing Edge Flap for Aeroelastic 'In-flight' Shape Optimization Tests [D] . Precup, Nathan 2018

机译：主动可变弯度连续后缘襟翼风洞模型的设计与构建，用于气动弹性“飞行中”形状优化测试
6. Modelling of mixed chemostat cultures of an aerobic bacterium Comamonas testosteroni and an anaerobic bacterium Veillonella alcalescens: comparison with experimental data. [O] . J Gerritse, F Schut, J C Gottschal 1992

机译：有氧细菌Comamonas testosteroni和厌氧细菌Veillonella alcalescens混合化学恒温培养的建模：与实验数据的比较。
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

Aeroelastic testing of LCA wing models - Model fabrication - Ground testing - Wind tunnel testing and Data analysisud

摘要

著录项

相似文献

相关主题

期刊订阅