翼身結構 的英文怎麼說

中文拼音 [yìshēnjiēgòu]
翼身結構 英文
wing-body configuration
  • 翼 : Ⅰ名詞1 （翅膀） the wing of a bird 2 （像翅膀的東西） the wing of an aeroplane etc : 鼻翼 wing of...
  • 身 : Ⅰ名詞1 （身體） body 2 （生命） life 3 （自己; 本身） oneself; personally 4 （人的品格和修養） on...
  • 結 : 結動詞（長出果實或種子） bear （fruit）; form （seed）
  • 構 : Ⅰ動詞1 （構造; 組合） construct; form; compose 2 （結成） fabricate; make up 3 （建造; 架屋） bui...
  • 結構 : 1 （各組成部分的搭配形式） structure; composition; construction; formation; constitution; fabric;...
  1. " the front of the car will be different, as far as the monocoque is concerned, with differently shaped sidepods, and the wing will be new too

    「只要改動將涉及單體橫造結構，前車身將會有所不同，不同的側箱結構，翼篇也將是全新的。 」
  2. Flutter analysis of a high - aspect - ratio sandwich wing under large angle of attack

    大展弦比飛機翼身結構不同剛度對結構響應的影響
  3. These advantage make it excellent materials for control surface, wing and skin of airplane

    是飛機結構中對剛度要求較高的操縱面、機翼和機身蒙皮結構用較理想的材料。
  4. Effects of different stiffness between wing and fuselage structures on structural responses for high aspect ratio airplanes

    無人機大展弦比直機翼單雙機身布局對結構剛度的影響
  5. This creates a second set of wings below the body and behind the arm wings, which is " a more anatomically and aerodynamically stable configuration ", he believes

    他認為，這樣就在身體下面和前翼後面構成了第二對翅膀，從解剖學和空氣動力學的意義上來說，這是更加穩定的結構。
  6. According to the design scheme of dishing axial - symmetric unmanned helicopter, the configuration and preliminary parameters are determined, and the general performance characteristics of the helicopter has been computed

    初步設計了碟形無人直升機的機身外形、旋翼系統、操縱系統，對全機總體結構進行了布置。
  7. Second, taking the characteristics of the mrfd and its matching with blades into consideration, the squeeze mode mrfd was designed. after that, the mechanical characteristics of the squeeze mode mrfd was tested to tell us that, compared with those mrfd work in other modes, the squeeze mode is advantageous for its compact structure, less displacement and higher strength. third, with the test data, we get the force model which use imitatation

    其次，考慮磁流變阻尼器自身特點與直升機旋翼的匹配因素，設計了以擠壓模式為工作方式的磁流變減擺器，並對磁流變減擺器進行了力學特性試驗，試驗結果表明擠壓式磁流變阻尼器與其他工作模式的磁流變阻尼器相比具有結構緊湊、位移小、出力大等優點。
  8. Wing fuselage structure

    機翼機身結構
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