On the base of design for new fighter planes, a method for calculating and simulating transient heat load for cabins has been proposed.
以我国新一代战斗机的研制为背景 ,提出了高精度的飞机座舱瞬态热载荷的计算与仿真方法 。
Numerical Simulation of Heat Transfer in Aircraft Cabins;
飞机座舱温度场数值仿真研究
A method is investigated for structural noise reduction of aircraft cabin by elastic wave control concept.
研究通过控制飞机座舱结构振动的弹性波的传播来减少由振动产生的辐射噪声的方法。
This text to the domestic and international relevant airplane cabin pressure control system of the cultural heritage carried on a detailed reading, analyze currently at home and abroad concerning cabin pressure control system research of the progress and the present condition.
通过对国内外有关飞机座舱压力控制系统的文献进行了详尽的解读,本文分析了目前国内外关于座舱压力控制系统研究的进展和现状。
The Application of Military Cockpit LCD Devices;
座舱LCD器件的军事应用
Numerical simulation is carried out to study the flow field and thermal fields inside a training-plane s air-conditioned cockpit under different air inlet conditions.
对某型号教练机座舱在不同进气温度方案下的气流组织进行数值模拟,研究舱内空气湿度、人体散热率和衣服热阻等因素的影响,获取了座舱内速度场和温度场分布。
The G_1 method is proposed to determine the weight factors of the evaluation indexes of cockpit ergonomics.
提出采用G1法确定歼击机座舱工效学评价指标的权重系数,利用该方法针对歼击机座舱工效学评价指标体系中的部分指标,按其对飞行员操作工效影响程度大小的原则,对聘请的飞过多种型号歼击机的24名现役有经验飞行员进行了调查,依据调查结果计算出了指标的权重系数。
Objective To analyze human operational reliability,and to provide suggestions for design of controllers in spacecraft cabin.
目的分析飞船乘员座舱内航天员操作的可靠性,从而对乘员座舱内手控设备的改进提供建议。