The big challenge is figuring out how to design the air intakes to maximize airflow over the fuselage.
最大的挑战是如何设计进风口以使机身气流最大化。
The airplane is based on a design where the fuselage provides a significant part of the lift.
该飞机的机身设计提供了重要的升力。
Together they will design and build the box that ties together the wings in the fuselage-the largest structural part of the wings.
他们将共同设计和制造机身上连接侧翼的部分—机翼上最大的构件。
This design created a gap between the air intake and the forward fuselage, and requires six small beams to enhance the structure for high-speed flight.
这样的设计导致了机身与进气口之间有一个间隔，为了高速飞行而在之间使用了6条小加强筋以加固结构。
Simultaneously all the main parameters are determined according to the environment of fuselage airproof main frame and the design requirements in analyzing the rigidity and strength.
根据承力密封框的使用环境和设计要求，确定了对其进行刚度和强度分析时所需的各种主要参数；
Note the missing fuselage panels behind the cowling which were replaced by louvered panels of Chinese design and which distinguished Zero 3372 in subsequent photographs.
注意发动机罩后面那块丢失了的机身蒙皮已由中国机械师设计的百叶窗式散热口的蒙皮来替代了。这使得3372号‘零’战在下面的照片中非常容易区分。
Design technology for integration of air vehicle fuselage, propulsion system and lifting control surfaces to optimize aerodynamic performance throughout the flight regime of an unmanned air vehicle.
为了优化无人驾驶航空飞行器在整个飞行过程中的空气动力特性而使机身、推进系统和升力控制面一体化的设计技术。
This machine adopts steel plate welding structure, the fuselage using the finite element analysis and design, Vibratory stress Relief of internal stress, so that body stable and reliable.
液压剪板机采用钢板焊接结构，机身采用有限元分析设计、振动时效消除内应力，使机身稳定、可靠。
The method of optimization theory based on dual method was transplanted to design fuselage main frame, and the optimizing model of fuselage main frame was established.
将基于二次规划的准解析法优化理论应用于机身主要承力框的设计中，建立了机身主要承力框的优化模型。
This paper presents briefly the application of the "improved" fully stressed design (FSD) method to fuselage structure design.
本文扼要介绍了“改进的”满应力设计方法(FSD)在机身结构设计中的应用。
Rationality of the method is made sure by being compared design plot of bend moment with experiment plot of bend moment of certain airplane AFT fuselage.
通过对某型飞机后机身设计弯矩图和试验弯矩图的比较，说明了这一方法的工程合理性。
The effects of wing-fuselage fusion design parameter have been analyzed.
分析了翼身融合设计参数的影响。
The design for the small punch testing machine is carried out based on the WDW-5 universal testing machine which is selected as the base fuselage.
选择WDW-5万能试验机作为小冲杆试验机的基础机身，并在此基础上进行设计。
The results of this model provide an important foundation for fuselage and arresting hook device design.
该模型的结果为机身和拦阻钩装置的设计提供了重要依据。
Germany's Flight design is a professional design and manufacture of light sport aircraft manufacturers, the company produces all-composite fuselage of the ct series aircraft movement.
德国飞行设计公司是专业设计和生产的轻型运动类飞机的厂家，公司主要生产全复合材料机身的CT系列运动型飞机。
In the sample application of a fuselage structure, the design is basically convergedafter only five iterations.
在某机身结构的实例应用中，设计经五次迭代，基本收敛。
This series press is the design which carries on in the domestic and foreign new press foundation, used the steel plate welding fuselage, the rigidity has been good, the precision was stable;
该系列压力机是在吸收了国内外新型压力机优点的基础上进行重新设计的产品，采用了钢板焊接机身，刚性好，精度稳定；
There are four post frame molding press and two kinds of structure, the fuselage uses finite element analysis and optimization design of the structure, reasonable structure.
成型压机有四柱和框架二种结构，机身采用有限元件结构分析和优化设计，结构合理。
On the basis of the canard configuration a contour stealthy design including chiefly the wing, the fuselage and their connection type is projected.
在鸭式布局的基础上，对飞行器各部件及部件间的连接方式进行了外形隐身设计。
Using this design approach, a typical civil aircraft fuselage structural design with the shape parameters of the cabin floor struts, cargo floor and foam components has been studied as design case.
采用该设计方法，以典型民机机身下部结构设计问题为算例，对客舱地板支撑结构，货舱地板和泡沫构件形状参数进行优化。
Using this design approach, a typical civil aircraft fuselage structural design with the shape parameters of the cabin floor struts, cargo floor and foam components has been studied as design case.
采用该设计方法，以典型民机机身下部结构设计问题为算例，对客舱地板支撑结构，货舱地板和泡沫构件形状参数进行优化。
应用推荐