静止スラストを最大とするロータ設計法

DOI Web Site Web Site 参考文献1件
  • 原田 正志
    連絡先著者（Corresponding author）：harada@chofu.jaxa.jp 宇宙航空研究開発機構

書誌事項

タイトル別名
  • Design Method of Maximum Static Thrust Rotor
  • セイシ スラスト オ サイダイ ト スル ロータ セッケイホウ

この論文をさがす

説明

In this paper, the practical design method of the maximum static thrust rotor based on the vortex method is described. After the vortex method is introduced, the simplified optimum rotor design method is presented. By analyzing the shape of the rotor wake, it was evident that the pitch of the vortices produced by the tip of the rotor is half that of the inboard vortices. The wake contraction rate parameter and axial vortex trajectory parameters are obtained from the tip vortices simulation. The accurate design method based on the vortex method with accurate wake model is then executed. The obtained maximum thrust rotor satisfies the conditions required on the Trefftz plane, which is not unfulfilled achieved by the simplified design method.

収録刊行物

参考文献 (1)*注記

もっと見る

キーワード

詳細情報 詳細情報について

問題の指摘

ページトップへ