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Application and Investigation of Configuration for Helicopter Engine Air Intake Based on Composites
Author(s): 
Pages: 56-59,63
Year: Issue:  z1
Journal: Aeronautical Manufacturing Technology

Abstract: 以某民用直升机发动机复合材料进气道构型设计为例,阐述和分析了基于复合材料的直升机发动机进气道构型的设计特点、进气道防砂网抗鸟撞构型研究以及旁通量设计等技术要求.
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