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Analytical Model for Ring-Wing Propulsor Thrust Augmentation
Journal of Aircraft ( IF 2.2 ) Pub Date : 2020-09-01 , DOI: 10.2514/1.c035922 M. J. Werle 1
Journal of Aircraft ( IF 2.2 ) Pub Date : 2020-09-01 , DOI: 10.2514/1.c035922 M. J. Werle 1
Affiliation
A simple, accurate, reduced-order model is developed for predicting the maximum available thrust performance of subsonic ring-wing propulsors varying in shroud airfoil length, thickness, camber, an...
中文翻译:
环形翼推进器推力增加的解析模型
开发了一个简单、准确、降阶的模型,用于预测亚音速环翼推进器的最大可用推力性能,这些推进器在护罩翼型长度、厚度、弯度、...
更新日期:2020-09-01
中文翻译:
环形翼推进器推力增加的解析模型
开发了一个简单、准确、降阶的模型,用于预测亚音速环翼推进器的最大可用推力性能,这些推进器在护罩翼型长度、厚度、弯度、...