T-tail flutterQuadratic mode shape componentsCFD unsteady aerodynamicsLinearized frequency domain CFDIt is known that the dynamic aeroelastic stability of T-tails is dependent on the steady aerodynamic forces at aircraft trim condition. Accounting for this dependency in the flutter solution process ...
T-tail flutter simulations with regard to quadratic mode shape components It is known that the dynamic aeroelastic stability of T-tails is dependent on the steady aerodynamic forces at aircraft trim condition. Accounting for this... D Schfer - 《Ceas Aeronautical Journal》 被引量: 0发表: 2021...
Surrey keeps calm over t-tail 'flutter' While most initially believed pitch-up was caused by the swept-back wings, I personally thought it was the wing that blanked-out flow over the T-tail (elevators) at high AoAs. Flight testing at Edwards AFB in the 1950s A new T-tail configuration...
The paper describes an experiment to measure steady lift loads on a T-tail flutter model. The method of test has been adapted from a technique used for measuring loads on aircraft in flight. A way of correcting the measurements has been devised. The measurements obtained are shown to explain...
2.Due to the special structure and aerodynamic configuration, the flutter characteristic analysis of T-tail empennage is complicated and the flutter speed is influenced by flight condition and some parameters that had been omitted, e.由于T型尾翼特殊的结构和气动布局形式,其颤振特性的分析比较复杂,飞行...
2.Due to the special structure and aerodynamic configuration, the flutter characteristic analysis ofT-tailempennage is complicated and the flutter speed is influenced by flight condition and some parameters that had been omitted, e.由于T型尾翼特殊的结构和气动布局形式,其颤振特性的分析比较复杂,飞行状态...
T尾 1. Effect of Mistuned Parameters on Mode Localization ofT-tailStructure 失调参数对T尾结构振动模态局部化的影响 2. Flutter Analysis ofT-tailAccording to the Different Supporting Stiffness T尾不同支持刚度的颤振分析研究 更多例句>> 2) T-tail ...
2. Flutter Analysis of T-tail According to the Different Supporting Stiffness T尾不同支持刚度的颤振分析研究 更多例句>> 6) T-head extrusion T形机头挤塑补充资料:尾形光琳 尾形光琳(1658～1716)Ogata Kōren 日本画家,工艺美术家。生于京都御用的和服商家庭,1716年6月2日卒于京都。早年随其父尾形宗...
Flutter Riverpod 消除多个依赖提供者问题描述 投票:0回答:1如Riverpod 文档中所述,Riverpod 提供商可以监视其他提供商来创建“处理管道”。 我有这样的东西: final prov = Provider<String>((ref){ final w1 = ref.watch(prov1); final w2 = ref.watch(prov2); final w3 = ref.watch(prov3); final w4...
Flutter of T-tail configurations is caused by the aeroelastic coupling between the vertical fin and the horizontal stabiliser. The latter is mounted on the fin instead of the fuselage, and hence the arrangement presents distinct characteristics compared to other typical empennage setups; specifically,...