This paaer presents selected results from several investigations of ari inlet design and performance. Diagnodtic data are from airfame-inlet model wind tunnel tests and CFD simulations.
提供的结果来自飞机进气道的设计和性能研究，分析所用的数据来源于进气道模型风洞实验和CFD数值模拟。
The experimental data of recent X-43A flight tests indicate that impulse wind tunnel could be used to predict a vehicle's flight performance.
近期美国X-43A的飞行试验数据表明脉冲式风洞能够预测飞行性能。
Furthermore, the buffet boundary correlation for the JL-6 aircraft was analyzed using the data obtained from wind tunnel tests and the flight test data of the JL-6 aircraft.
利用风洞试验和飞行试验得到的数据进行了JL - 6飞机抖振边界相关性分析。
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