大気吸込式衝撃風胴を使用した翼列流れの圧力計測

DOI Web Site Web Site

書誌事項

タイトル別名
  • Pressure Measurement of Flow through Cascade Using the Suction-Type Shock Tunne
  • タイキ スイコミシキ ショウゲキ フウドウ オ シヨウシタ ヨクレツ ナガレ

この論文をさがす

抄録

This paper describes a pressure measurement method of the transonic flow through the turbine cascade by means of the suction-type shock tunnel.<BR>The present method which uses silicon oil containing tubes is characterized by an improvement in the response of the pressure-time. It is shown that the values of the static pressures on the blade surfaces measured by the present method almost agree with those by the optical method. The experimental results using a Pitot tube are also shown as an example of this method in order to obtain the total pressures downstream of the cascade.

収録刊行物

詳細情報 詳細情報について

問題の指摘

ページトップへ