摘要: Because of one engine inoperative requirements, together with hot-gas reingestion and hot day, high altitude takeoff situations, power augmentation for multiengine rotorcraft has always been of critical interest. However, power au... 展开
作者 | biesiadny, t. j. klann, g. a. | ||
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原报告号 | N8720280 | 总页数 | 14 |
报告类别/文献类型 | NASA / NTIS科技报告 | ||
关键词 | Engine coolants Rotary wing aircraft Turboshafts Water injection Contingency Engine tests Horsepower Augmentation Engine failure Helicopters Temperature control Turbine blades |