A sim.le pressure-gain com.ustor, without m.ving parts, which has been shown to produce a stagnation pressure-gain across the com.ustor in excess of 5 percent at a com.ustor stagnation tem.erature of 3:1 is described....
详细信息
A sim.le pressure-gain com.ustor, without m.ving parts, which has been shown to produce a stagnation pressure-gain across the com.ustor in excess of 5 percent at a com.ustor stagnation tem.erature of 3:1 is described. It should be possible to incorporate com.ustors based on the prototype in m.ny gas turbines.
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