On a Theory of Shock Waves in Locally Supersonic Zone and a New Boundary-value Problem for Tricomi's Equation

スポンサーリンク

概要

• 論文の詳細を見る

• The hodograph behavior of the shock wave in transonic flow with nonuniform initial state is discussed. Besides the shock polar, two conditions are derived which, as a special case, comprise Busemann's spine and serve to eliminate the indeterminateness which constitutes specific difficulty for the treatment of high subsonic flow with shock waves. Applying these three equations to the transonic flow over an airfoil, a new boundary-value problem is proposed. The problem still involves indeterminateness, but in a special case when the airfoil has a ridge it can be simplified so as to develop further analysis.

• 社団法人日本物理学会の論文
• 1957-12-05

著者

• Tsuge Shun-ichi

  Department Of Aeronautics Faculty Of Engineering University Of Tokyo

関連論文

• On a Theory of Shock Waves in Locally Supersonic Zone and a New Boundary-value Problem for Tricomi's Equation

スポンサーリンク