On the Subsonic Flow behind the Bow Wave of a Finite Wedge

スポンサーリンク

概要

• 論文の詳細を見る

• Recently K. Tamada analysed the subsonic flow over a finite wedge behind the attached shock wave by solving a linearized potential equation by an ingenious method. When the shock is not strong, the linearized potential equation may be applied with good approximation. But, when the shock is strong, the flow field behind the shock should be treated as an anisentropic and rotational one. For such an anisentropic flow Lighthill's equatioh will be more suitable. By the use of Lighthill's equation we obtained an analytical expression of the problem in a form analogous to Tamada's one. Futhermore, we also analysed the ease for a finite wedge whose surface deviates slightly from a straight line.

• 社団法人日本物理学会の論文
• 1954-04-25

著者

• Oguchi Hakuro

  Institute Of Science And Technology University Of Tokyo

関連論文

• Large-Eddy Structures in a Turbulent Mixing Layer
• On the Subsonic Flow behind the Bow Wave of a Finite Wedge
• Supersonic Jet with the Ambient Pressure corresponding to its Constant Pressure Point
• On the Attached Curved Shock in Front of an Open-Nosed Axially Symmetrical Body

スポンサーリンク