Our official English website, www.x-mol.net, welcomes your
feedback! (Note: you will need to create a separate account there.)
Slowed Hingeless Rotor Wind Tunnel Tests and Validation at High Advance Ratios
Journal of Aircraft ( IF 1.5 ) Pub Date : 2021-01-01 , DOI: 10.2514/1.c035900 Xing Wang 1 , André Bauknecht 2 , Shashank Maurya 1 , Inderjit Chopra 1
Journal of Aircraft ( IF 1.5 ) Pub Date : 2021-01-01 , DOI: 10.2514/1.c035900 Xing Wang 1 , André Bauknecht 2 , Shashank Maurya 1 , Inderjit Chopra 1
Affiliation
In forward flight, slowing down a rotor alleviates compressibility effects on the advancing side blade tip, extending the cruise speed limit, and inducing high-advance-ratio flight regime. Previous...
中文翻译：
低速无铰转子风洞试验和高提前比下的验证
在前飞中，减慢旋翼可减轻对前进侧叶尖的可压缩性影响，延长巡航速度限制，并诱导高前进比飞行状态。以前的...
更新日期：2021-01-01
中文翻译：
低速无铰转子风洞试验和高提前比下的验证
在前飞中，减慢旋翼可减轻对前进侧叶尖的可压缩性影响，延长巡航速度限制，并诱导高前进比飞行状态。以前的...
京公网安备 11010802027423号