The particularity of the altitude simulated test of an engine with Laval nozzle was analyzed in brief. The engine thrust determination and correction in altitude test with large deviation of simulated ambient pressure was put forward.
英
美
- 簡(jiǎn)析了拉瓦爾噴管發(fā)動(dòng)機高空模擬試驗的特殊性,提出了大模擬偏差條件下確定和修正拉瓦爾噴管發(fā)動(dòng)機推力的方法。