首页> 美国政府科技报告 >Flutter experiences with thin pointed-tip wings during flight tests of rocket-propelled models at Mach numbers from 0.8 to 1.95

【24h】

Flutter experiences with thin pointed-tip wings during flight tests of rocket-propelled models at Mach numbers from 0.8 to 1.95

机译：在马赫数为0.8至1.95的火箭推进模型的飞行试验中，薄尖尖翼的颤振经验

获取原文

页面导航

摘要
著录项
相似文献
相关主题

摘要

No Abstract Available

著录项

作者
Wallskog, Harvey A;
展开▼
作者单位

展开▼
年度 1955
页码 1-32
总页数 32
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. MATLAB-Based Flight-Dynamics and Flutter Modeling of a Flexible Flying-Wing Research Drone [J] . Schmidt David K. Journal of Aircraft . 2016,第4期

机译：基于MATLAB的柔性飞行翼无人机的飞行动力学和颤振建模
2. 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
3. T-tail flutter: Potential-flow modelling, experimental validation and flight tests [J] . Joseba Murua, Pablo Martinez, Hector Climent, Progress in Aerospace Sciences . 2014,第nova期

机译：T尾颤振：势流建模，实验验证和飞行测试
4. Flight Testing Flutter Suppression on a Small Flexible Flying-Wing Aircraft [C] . Brian P. Danowsky, Aditya Kotikalpudi, David K. Schmidt, AIAA/ISSMO multidisciplinary analysis and optimization conference;AIAA aviation forum . 2018

机译：在小型柔性飞翼飞机上进行飞行测试颤振抑制
5. Flight flutter testing - Advanced methodologies [D] . Desforges, Matthew J. 1995

机译：飞行颤振测试-高级方法
6. Modeling and Closed Loop Flight Testing of a Fixed Wing Micro Air Vehicle [O] . Harikumar Kandath, Jinraj V. Pushpangathan, Titas Bera, 2018

机译：固定翼微型飞行器的建模和闭环飞行测试
7. Force Measurements on a Body wing tail configuration (KaHa Model) at Mach numbers of 0.4 , 0.6 and 0.8 and incidences from 30° to 65° [O] . Kanagarajan V, Hartmann K 1988

机译：马赫数为0.4，0.6和0.8且入射角为30°至65°的机翼尾翼构型（KaHa模型）上的力测量

Flutter experiences with thin pointed-tip wings during flight tests of rocket-propelled models at Mach numbers from 0.8 to 1.95

摘要

著录项

相似文献

相关主题

期刊订阅