日本航空宇宙学会論文集
Online ISSN : 2432-3691
Print ISSN : 1344-6460
ISSN-L : 1344-6460
論文
有限な斜面上でホバリングするロータの地面効果とブレードフラッピング運動
井星 正氣糸賀 紀晶長島 知有Daniel P. SchrageJ. V. R. Prasad
著者情報
ジャーナル フリー

2002 年 50 巻 582 号 p. 264

詳細
抄録

To grasp effects of such ground effect parameters as rotor height, ground inclination angle, and location of the rotor hub center from the edge of ground plane, on blade flapping motion of a rotor hovering above finite inclined ground plane, a hovering test of the rotor was conducted using a finite ground effect plate and a model rotor. The thrust, torque, and blade flapping motion of the hovering rotor were measured for a wide variety of ground effect parameters. A very unique behavior of the blade flapping motion due to flow separation around a finite ground effect plate edge is clarified.

著者関連情報
© 2002 The Japan Society for Aeronautical and Space Sciences
前の記事 次の記事
feedback
Top