A Simplified Method Calculating The Laminar Boundary Layer

スポンサーリンク

概要

• 論文の詳細を見る

• A some what simplified method calculating the steady and incompressible laminar boundary layer flow is developed basing on the "local similarity". The analysisis performed by using the variables proposed by Goertler. The calculated results are utilized to predict the separation points in some decelerated flows and the comparison with other exact solutions shows that the value of the "similar parameter" may be taken as -0.224 at the separation points in this method.

• 社団法人日本物理学会の論文
• 1961-04-05

著者

• Kawamata Shin

  The Aeronautical Research Institute University Of Tokyo

• Kawamata S.

  The Aeronautical Research Institute, University of Tokyo

関連論文

• A Simplified Method Calculating The Laminar Boundary Layer

スポンサーリンク