要在一个可控的落围内产生高温和高压，可测量的方法成为重现聚变的最大障碍。
Replicating the scorching temperatures and intense pressures of this process in a controlled, measurable way was one of the biggest obstacles to replicating fusion.
指出，当超音速飞行时，在前喷管附近的弹体表面上产生一个局部高压区，由此形成一个翻转力矩。
It is demonstrated that there exists a part of high pressure on the body surface of the rocket near the fore-located nozzles, thus forming a overturning moment.
应用推荐