panel aircraft 中文意思是什麼
panel aircraft
解釋
裝有隨機工程師認儀錶板的飛機-
The result was shown that the program runs quickly and in reliability, it can replace the nomograph method and use easily for predicating sonic fatigue life of aircraft skin - panel structure
通過已有的算例進行驗證，結果表明計算迅速可靠，可以代替以列線圖為主要手段的求解方法，廣泛的應用於工程領域。 -
Dynamic finite - element simulation on aircraft panel structure battle damage
飛機壁板結構戰傷的動力有限元模擬 -
The applications on chinese aircrafts showed the validity of the proposed numerical method in aircraft panel
該軟體先後在「梟龍」戰斗機和「某型號」運輸機上成功應用，前一型號已經在03年9月成功首飛。 -
Integral panel is a flat part integrated with framework elements, connection elements and skin in traditional aircraft structure, it is the main supporting structure in aircraft, having the advantages of high - intensity, low - weight, and so on
整體壁板是將傳統飛機結構中的骨架元素、連接元素和蒙皮製成一體的板類零件，是飛機的主要受力結構件，具有強度高、重量輕、氣密性好等優點。 -
Aircraft instrument panel
飛機儀錶板 -
In first part of the thesis, by a review of the research on aircraft sonic fatigue, the formulas for calculating natural frequencies of the typical aircraft skin - panel structure with four edges simply - supported or four edges fixed - supported were drawn, the response of displacement and stress was analysed under the condition of random white noise loading with the steady - state or unsteady - state. the procedure how to use data of s - n curve under constant loading for predicating the fatigue life of skin - panel subjected to random loading was shown
通過對聲疲勞問題研究的回顧，根據典型飛機蒙皮壁板模型，整理了四邊固支，四邊簡支兩種邊界條件下多階模態固有頻率，非平穩及平穩隨機白噪聲載荷下的位移和應力響應，以及如何從等幅s ? n曲線求得隨機載荷應力下的疲勞壽命。 -
Finally, an iterative method coupled between rotor free wake model and lifting wing panel model is given. by the method, the aerodynamic interaction of the rotor on its wing for tilt - rotor aircraft in hover are computed and discussed
最後，建立了一個耦合的旋翼機翼氣動干擾分析方法，計算分析了懸停狀態旋翼流場對機翼的氣動干擾影響。 -
Based on the analysis of advanced composite structure design and its optimal methods, the author in this thesis sophisticatedly discusses the applied optimal design techniques of composite layered panel tail - structure of a developing aircraft in the phase of theoretical layout design by using ansys system
本文在分析復合材料結構設計技術及優化設計方法的基礎上，應用ansys軟體環境，系統深入地研究探討了某型在研飛機平尾復合材料結構打樣設計階段的實用優化設計技術。 -
The selection of material, typical the structural designs, the mechanical property and the forming pressure of unmanned aircraft sandwich composite material have been studied in this paper. it has analysed and discussed the flexural properties of honeycomb sandwich plate delamination under bending loads in detail. and then the mechanical properties of the laminate panel are studied which are compared with honeycomb sandwich panel
在圍繞某無人機蒙皮選用材料的基礎上，重點對蜂窩夾層結構的結構設計、力學性能、成型壓力對力學性能的影響，以及缺陷對蜂窩夾層結構復合材料的彎曲性能影響進行了較深入的實驗研究和理論分析，同時比較了蜂窩夾層結構中面板與同樣材料鋪層的疊層板力學性能的差異。 -
The director of civil aviation, mr albert lam today ( november 3 ) showed several members of the legislative council ( legco ), most of whom are members of the panel on economic services, the air traffic control ( atc ) operation at the hong kong international airport ( hkia ) and the state - of - the - art equipment used in training air traffic control officers ( atcos ) to ensure a safe and efficient flow of aircraft movements in and out of hong kong
立法會議員參觀民航處設施二年十一月三日民航處處長林光宇今日（十一月三日）向多位立法會議員（主要為經濟事務委員會委員）介紹香港國際機場航空交通管理運作，並且展示用作培訓航空交通管制主任以確保香港航空交通安全暢順的先進設備。 -
Adrepp aircraft accident data reporting panel
飛機事故數據報道組聯合國
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