摘要
针对某型电子侦察机天线罩，计算得出飞机在飞行过程中天线罩的结冰区、结冰量及其在结冰区内的分布，并利用冰风洞进行了模拟实验，为天线罩有效防冰提供了可靠的理论依据。
The icing scope, amount and distribution within the scope are calculated for an aerial cover of an electron detective plane which is flying, and an imitation experiment using an icing wind tunnel has been done, which supplies a reliable theoretical foundation for the aerial cover anti icing effectively.
出处
《航空学报》
EI
CAS
CSCD
北大核心
1997年第4期423-426,共4页
Acta Aeronautica et Astronautica Sinica
关键词
飞机防冰
撞击特性
结冰区
结冰量
天线罩
anti icing of airplane, impingement characteristics, icing area, amount of ice
