本文讨论了构成气动数据处理装置及气动模拟计算装置中几种器件的可能方案。
In this paper possible schemes for constructing several devices used in pneumatic data-processing equipments and pneumatic analog computing equipments are discussed.
系统关键技术含气动数据结构的设计、数据的标准化表示、数据的对比分析及模型数据的前置处理。
The key techniques of system include design of data structure, standardization of data expression, data comparative analysis and pre-process of model data.
然而，Darpa表示，在以17到22倍音速飞行的状态下，飞机还是回传了139秒的空气动力学数据。
However, the flight still managed to return 139 seconds of aerodynamic data at a velocity between 17 and 22 times the speed of sound, Darpa said.
不过，他们至少还有三年半的时间收集上层大气动力的有效数据。
They will have at least three and a half more years, though, to gather good data on upper atmospheric dynamics.
研究静气动弹性问题一大关键是要解决流固数据耦合。
Realizing data exchange to reflect coupling between fluid and structures is essential to solving static aeroelasticity problems.
论文主要研究从弹丸自由飞行数据中如何准确地拟合空气动力系数。
This paper mainly studies how to accurately fit the air dynamics parameter by the ballistic data of projectiles' free flight.
为了提高气动参数辨识的精度，根据飞机运动方程，给出了测量中的系统偏差、尺度因子误差和随机噪声描述，并提出了一种飞行数据相容性检验的快速算法。
To get high accuracy of the identification of aerodynamic parameters, based on the motion equation of an aircraft, a fast algorithm for flight data compatibility check is presented in this paper.
本文以风洞试验数据为依据，对在任意方向水平作用下的机身、垂尾和尾桨气动特性进行了研究。
This peper is based on the wind tunnel experiment data and studies the air dynamic performance of fuselage, horizontal stabilizer and fin under level wind in any direction.
本文通过高真空气动挡板阀的数据分析来说明漏率和升压率在高真空范围内二者之间的差异。
The difference between leak rate and rate of pressure rise of high vacuum pneumatic operation baffle valve is analyzed.
根据理论与试验两方面的数据，总结了阻性消声器的空气动力性能。
The aerodynamic quality of dissipative silencer is summarized through the data from theory and experiment.
比较了穿衣袖与不穿衣袖两种状态下手臂的气动力数据。
Aerodynamic data on upper arm were compared under the conditions with and without cloth.
本文概述最初阶段利用风洞试验数据应用模糊逻辑研究飞机大攻角空气动力学的情况。
In this paper, the initial stage in application of fuzzy logic to aircraft high-Angle-of attack aerodynamics using wind tunnel test data is outlined.
计算了颗粒与气体不同温差情况下高温颗粒的气动阻力，并根据计算数据点拟合了计算公式。
Then compute aerodynamic drag of high temperature particle at different temperature difference and fit the formula according to the computational data points.
返回舱飞行试验的配平气动特性可从舱内惯性平台的加速度和姿态记录数据以及轨道数据求出。
The flight trim aerodynamic characteristics of re-entry modules were calculated from on board-recorded inertial-platform accelerations and attitudes and from reconstructed trajectory data.
在气动热计算中，应直接观察热流数据的收敛，确保得到真正的收敛解。
In order to get the convergence solution it is necessary to monitor the convergence of heat transfer data directly.
根据测量数据计算出尾梁上气动力随环量控制参数的变化情况，并绘制成曲线。
The aerodynamic forces on the tail boom have been calculated and their changes with the circulation control variables were drawn in curves.
计算出的空气动力数据与实验结果吻合。
Calculated values of the aerodynamical loads on a tangent-ogive forebody compare well -with experimental data.
计算结果符合基本气动力规律，和实验数据基本吻合。
The calculated results accord with the aerodynamic theory as well as the data of the experiment.
对飞行器及其部件进行气动力数值模拟时，气动外形常常是以离散数据形式给出。
When aerodynamic numerical simulation for flight vehicle and its components is conducted, the aerodynamic shape is generally given in the manner of discrete data.
拟设计开发一套便携稳定、低功耗的数据采集、无线监测系统用于列车空气动力学测试试验。
In order to have test on high-speed train aerodynamics, we would like to Design a portable, stable and low-power data acquisition and wireless monitoring system.
气动性能计算为气动设计结果提供评价和反馈，并为叶片的结构设计提供气动载荷的原始数据。
Aerodynamic performance calculation provides evaluation and feedback for the aerodynamic design and also the aerodynamic load data for the structural design of blade.
大规格气动执行机构与手动机构，如用户有特殊要求，可提供数据定制。
Large specification of Pneumatic operation organ and manual organ. If users have special requirements, we can make according to the provided data.
气动力数值模拟系统是CFD流场解算技术、网格生成技术、数据可视化技术和网络技术相结合的产物。
CFD numerical simulation system is a combined technology of CFD flow solving, grid generation, data visualization and networking.
气动力数值模拟系统是CFD流场解算技术、网格生成技术、数据可视化技术和网络技术相结合的产物。
CFD numerical simulation system is a combined technology of CFD flow solving, grid generation, data visualization and networking.
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