摘要
根据进气道旋流产生的机理，从进气道设计方面，较为全面地研究了现存飞机进气道旋流的一些防止和抑制措施，将有益于解决工程上由于旋流而造成的进气道与发动机的流场匹配方面的问题。
Based on the mechanicsm of inlet swirl, the measures to prevent andrestrain the inlet swirl of present aircraft in an all-round way from the inlet designpoint of view are studied' It is hoped that the author's thinking will benefit the solution of the problems in engine/inlet compatibility arising from swirl'
出处
《推进技术》
EI
CAS
CSCD
北大核心
1994年第2期17-24,共8页
Journal of Propulsion Technology
关键词
歼击机
航空发动机
进气道
匹配
Fighter aircraft,Aircraft engine,Inlet-engine matching,Inlet flow,Flow distribution,Flow distortion
