论文信息 - Effect of Small Angles of Attack on Laminar-Turbulent Transition in the Supersonic Boundary Layer on a Swept Wing with χ = 72° - 字舞流文

Effect of Small Angles of Attack on Laminar-Turbulent Transition in the Supersonic Boundary Layer on a Swept Wing with χ = 72°

A. Kosinov | A. Semenov | Y. G. Ermolaev | N. Semionov | V. Kocharin | A. Yatskikh | S. A. Shipul’