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起飞性能
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  take-off performance
     Research on Take-off Performance of the MA60 Aircraft at Plateau Airport
     MA60飞机高原机场起飞性能研究
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     The Influence of Thrust Vectoring on Aircraft Take-Off Performance
     推力矢量飞机的起飞性能研究
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     Analysis on Ski-Jump Take-off Performance for a Fighter
     某型战机滑跃起飞性能初步分析
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     The results shows, after optimization, the ski jump take-off performance is improved to a great extent.
     计算结果表明,对斜板形状进行优化后,可以在很大程度上提高舰载机的斜扳滑跃起飞性能
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     This paper gives a research on the take-off performance of the MA60 aircraft at plateau airport,which is self-made wholly by China.
     针对我国自行研制的支线飞机———MA60飞机进行了高原机场起飞性能研究。
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  takeoff performance
     This paper presents a general programme in computer language FORTRAN for calculating the take off performance of commercial jet airliners, taking the Boeing 767 200 (JT9D 7R4E) as a successful example.
     介绍了用 F O R T R A N 语言编写的喷气式旅客机起飞性能计算的通用程序,并以 B767200( J T9 D7 R4 E)为例,成功地计算了该机型的起飞性能
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     This paper analyzes the different deflexion angle of thrust vectoring influence on aircraft take off performance according to the result of numerical simulation.
     通过数值仿真探讨了推力矢量的偏转大小对起飞性能的影响 ,对不同推力矢量偏转下飞机起飞性能的仿真计算结果进行了分析。
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     The result indicate that direct force can improve take off performance obviously.
     仿真结果表明 ,采用直接力控制可以明显提高飞机的起飞性能
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     Designing a General Programme for Calculating the Take off Performance of Commercial Jet Airliners
     喷气式旅客机起飞性能计算通用程序设计
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     For correct and wide application of reduced thrust takeoff technique,the temperature characteristics of high bypass ratio turbofan engines and the takeoff performance of large aircrafts were analyzed.
     为正确使用和推广减推力起飞技术,分析了高涵道比涡轮风扇发动机温度特性和大型民航机起飞性能.
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  take off performance
     This paper presents a general programme in computer language FORTRAN for calculating the take off performance of commercial jet airliners, taking the Boeing 767 200 (JT9D 7R4E) as a successful example.
     介绍了用 F O R T R A N 语言编写的喷气式旅客机起飞性能计算的通用程序,并以 B767200( J T9 D7 R4 E)为例,成功地计算了该机型的起飞性能
短句来源
     This paper analyzes the different deflexion angle of thrust vectoring influence on aircraft take off performance according to the result of numerical simulation.
     通过数值仿真探讨了推力矢量的偏转大小对起飞性能的影响 ,对不同推力矢量偏转下飞机起飞性能的仿真计算结果进行了分析。
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     The result indicate that direct force can improve take off performance obviously.
     仿真结果表明 ,采用直接力控制可以明显提高飞机的起飞性能
短句来源
     Designing a General Programme for Calculating the Take off Performance of Commercial Jet Airliners
     喷气式旅客机起飞性能计算通用程序设计
短句来源
     For correct and wide application of reduced thrust takeoff technique,the temperature characteristics of high bypass ratio turbofan engines and the takeoff performance of large aircrafts were analyzed.
     为正确使用和推广减推力起飞技术,分析了高涵道比涡轮风扇发动机温度特性和大型民航机起飞性能.
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  “起飞性能”译为未确定词的双语例句
     THE EFFECTS OF DECK'S LONGITUDINAL SHAKING ON LAUNCHING PERFORMANCE
     舰面纵摇对弹射起飞性能的影响
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     Based on the analysis on the operating charateristies of the waterinlet for hydrofoil water-jet propulsion system,the inherent short-coming of the conventional water-inlet(with an invariable inlet area),which can not obtain the optimum foilborne and taking-off performan-cec of the hydrofoil is discussed,and a kind of new adjustable waterinlet is then introduced.
     本文在分析水翼艇喷水推进系统进水口工作特点的基础上,论述了常规的固定式进水口不能保证艇同时得到最佳的翼航和起飞性能这一固有弊病,提出了可以用可调进水口的方案。
短句来源
     Finally, a brief discussion is present about the influence of the airplane gross weight, the thrust, the maximum angle of attack, the flap angle and the wind over the deck on the catapulting performence.
     最后讨论了飞机的起飞质量,发动机推力、起飞迎角、襟翼偏角和甲板风航迹等对弹射起飞性能的影响.
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     This paper is directed against that Y-12(Ⅱ)aircraft’s main wheels au-tomatically appear the phnomenon leaving from ground in its flight test of takeoff per-formance with low weight. It discovered the primary reason,and put forward the methodand improvenment measure solved the problem. It also studied the influence factors foraircraft’s takeoff performane.
     针对Y─12(Ⅱ)型飞机在进行小重量起飞性能试飞时出现的主轮自动离地现象进行了讨论分析,找出了产生主轮自动离地现象的主要原因,提出了解决问题的方法和改进措施,并分析研究了对起飞性能的影响因素,为改善起飞操纵性提供了依据。
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     Finally, taking H6 aircraft as example, this article calculated the taking off performances of the aircraft under the condition of cross wind and high cross wind. It has a certain guidance function to the actual flight.
     并以H6飞机为例,计算了飞机在侧风、大侧风条件下的起飞性能,为各型飞机侧风起飞安全提供了理论依据,对实际飞行具有一定的指导作用。
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  take-off performance
An experimentally based dynamic model of the musculoskeletal system was employed to simulate the measured kinematics and reaction force data and to study the sensitivity of take-off performance to initial kinematic conditions.
      
Take-off performance under optimal and suboptimal thermal conditions in the butterfly Pararge aegeria
      
Guidance strategies for near-optimum take-off performance in a windshear
      
The way of the take-off performance is influenced by the changes in the equipment of the ski jumpers and by the differences in the technique.
      
  takeoff performance
As such, the configuration would incur the increased weight and decrease in CL with the associated detrimental effect on takeoff performance.
      
Because the trim moment is generated by a down force on the tail, any reduction in required moment directly improves takeoff performance.
      
  take off performance
The aircraft was also flown by the owner for a short hop along the runway to demonstrate its take off performance.
      


This paper describes the model tests of shallow water resistance and presents test result analysis of an inland river hydrofoil boat. The results show that the take-off characteristics are strongly influenced by shallow water effect. It is suggested that emphasis must be given to shallow water effect not only for ordinary inland rivet hydrofoil boats but also for some offshore ones. Much attention must be paid to wider range or shallow water depths instead of local depths. Detail charts of resistance increment...

This paper describes the model tests of shallow water resistance and presents test result analysis of an inland river hydrofoil boat. The results show that the take-off characteristics are strongly influenced by shallow water effect. It is suggested that emphasis must be given to shallow water effect not only for ordinary inland rivet hydrofoil boats but also for some offshore ones. Much attention must be paid to wider range or shallow water depths instead of local depths. Detail charts of resistance increment ratio, squat ratio and tilt ratio versus depth Froude number are given, together with equations of regressive analysis.

本文介绍对一艘内河水翼艇所作的浅水阻力模型试验及对试验结果的总结分析。结果表明,不仅普通内河水翼艇,就是某些沿海水翼艇也必须注意航道浅水效应对起飞性能的影响问题,而且需要特别注意的是在较大的浅水深范围,而不是在较小的浅水深范围。文中详细提供了有关图谱,对若干主要结果给出回归方程式。以便于应用和分析。

Based on the analysis on the operating charateristies of the waterinlet for hydrofoil water-jet propulsion system,the inherent short-coming of the conventional water-inlet(with an invariable inlet area),which can not obtain the optimum foilborne and taking-off performan-cec of the hydrofoil is discussed,and a kind of new adjustable waterinlet is then introduced.The effects of the conventional and adjustablewater inlets on the hydrofoil foilborne and taking-off performances arealso analysed.The full-scale tests...

Based on the analysis on the operating charateristies of the waterinlet for hydrofoil water-jet propulsion system,the inherent short-coming of the conventional water-inlet(with an invariable inlet area),which can not obtain the optimum foilborne and taking-off performan-cec of the hydrofoil is discussed,and a kind of new adjustable waterinlet is then introduced.The effects of the conventional and adjustablewater inlets on the hydrofoil foilborne and taking-off performances arealso analysed.The full-scale tests of the hydrofoil with the adjustablewater inlet give satisfactory results.

本文在分析水翼艇喷水推进系统进水口工作特点的基础上,论述了常规的固定式进水口不能保证艇同时得到最佳的翼航和起飞性能这一固有弊病,提出了可以用可调进水口的方案。在分析了进水口的设计要求后,介绍了实艇上采用可调进水口对其翼航和起飞性能的影响,取得了预期的满意效果。

This paper, by investigating the catapulting dynamics of the carrier-based airplane and according to the requirements of catapult takeoff, provided a method to determine catapulting parameters(the catapult force, the thrust and the elevator angle). In this paper, the take-off path of sea-based aircraft was calculated. Finally, a brief discussion is present about the influence of the airplane gross weight, the thrust, the maximum angle of attack, the flap angle and the wind over the deck on the catapulting performence....

This paper, by investigating the catapulting dynamics of the carrier-based airplane and according to the requirements of catapult takeoff, provided a method to determine catapulting parameters(the catapult force, the thrust and the elevator angle). In this paper, the take-off path of sea-based aircraft was calculated. Finally, a brief discussion is present about the influence of the airplane gross weight, the thrust, the maximum angle of attack, the flap angle and the wind over the deck on the catapulting performence.

本文通过舰载飞机弹射起飞动力学的研究,并根据弹射起飞的过程和要求,提出了确定弹射起飞参数(弹射力、发动机推力和平尾偏角)的计算方法。文中对舰载机的弹射起飞进行了仿真计算。最后讨论了飞机的起飞质量,发动机推力、起飞迎角、襟翼偏角和甲板风航迹等对弹射起飞性能的影响.

 
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