The paper investigates the problem on vortex generator controlboundary layer's separation of supercritical airfoil and wing for body configuration wing.
本文研究涡流发生器控制超临界翼型和翼身组合体机翼的附面层分离问题。
2
Based on forecast technique the time control models are built in the equipment engineering supervision. Then a novel method is proposed for the time controlboundary.
文章基于预测技术，建立了设备工程进度控制的模型，并提出了设备工程进度目标控制界限的确定方法。
3
Based forecast technique the quality control models are built in the equipment engineering supervision. Then a novel method is proposed for the quality controlboundary.