尾翼作用 的英文怎麼說
中文拼音 [wěiyìzuòyòng]
尾翼作用
英文
tail effect-
The forces on an isolated tail are represented just like those on an isolated wing.
作用在單獨尾翼上的力的表示方法正和單獨機翼的情形一樣。The main work in this paper includes three parts : the theory research on partially - cavitating and super - cavitating axisymmetric bodies, the numerical computations and experimental investigations on partially - cavitation and super - cavitation on axisymmetric bodies. after finishing the study of theory and experiment on the partially - cavitation and super - cavitation for axisymmetric body, i use the potential flow theory to build the mathematical model on the partially - cavitation and super - cavitation for axisymmetric body. many cavity wake models, such as pressure recovery close model, riabouchinsky model and re - entrant jet model, are studied seriously
本文在深入研究了回轉體局部空化與超空化理論及實驗結果的基礎上，基於勢流理論，建立了回轉體局部空泡和超空泡流場的基本數學模型，通過對kinnas和fine 、 uhlman以及jiedang和gertkuiper等人基於二維水翼提出的壓力恢復閉合模型、鏡像板模型和回射流模型等空泡尾流模型進行了逐一的研究分析，發現其中的壓力恢復閉合模型較適用於模擬回轉體空泡尾部流場，並選用此空泡尾流模型作為求解回轉體空化流場正問題與逆問題的數學模型的組成部分。The tail lift curve slope as determined from the panel model may require adjustment in order to apply the test results.
為了應用試驗結果，根據翼段模型試驗確定的平尾升力曲線斜率可能要作些修正。The material characteristic and principle of piezoelectric material ( pzt ) and macro - fiber composite ( mfc ) is analyzed. cada - x structural dynamics analytic software is used to carry on the experimental modeling and mode analysis of the vertical tail. consequently, the disposal scheme of sensor and actuator is confirmed
本文的主要研究內容為:一、分析了壓電陶瓷和壓電纖維復合材料的特性及工作原理，採用比利時lms公司的cada - x結構動力學分析軟體對尾翼模型進行實驗建模與模態分析，根據模態實驗結果，確定了傳感/驅動元件的布置方案。Abstract : on the basis of setting up the angle motion mathematic model of the terminal correct projectile forced by impulse corrective force, this paper discusses the dynamic response of the terminal correct projectile and response spectrum. the general conclusion that profit to design impulse correct projectile stabilized by taifl wing is given
文摘:建立了末段脈沖修正彈在脈沖修正力作用下的角運動數學模型，分析了末段修正彈對脈沖修正力的動態響應特性和響應譜，給出了對尾翼穩定脈沖修正彈設計有普遍指導意義的結果。分享友人