微粒子-気体衝撃波管内におかれた円柱を過ぎる衝撃波背後の流れ

概要

論文の詳細を見る
An experimental investigation was made of a shock wave induced flow past a circular cylinder in a dusty-gas shock tube. Joint research was conducted between the Muroran Institute of Technology and the Institute of High Speed Mechanics, Tohoku University. Shock tubes used for the present research have test sections of identical geometry. For a frozen shock Mach number of 1.3, flow visualization studies were conducted by a schlieren method and an Ime-Con High Speed Camera in Muroran and a pulsed laser holographic interferometer in Sendai. The behaviour of shock waves past a circular cylinder in a dusty-gas, the development of dust free regions and the formation of vortices behind a circular cylinder were observed in detail by those flow visualization methods.
一般社団法人日本機械学会の論文
1987-12-25