Numerical investigation of laminar separated viscous trailing-edge flow using triple-deck theory
Flight Simulation Technologies Conference and Exhibit ; 1990 ; Dayton , OH , U.S.A.
1990-01-01
Conference paper
Electronic Resource
English
Triple-deck theory of supersonic laminar viscous–inviscid interaction due to wall temperature jumps
Online Contents | 2007
|Wall-Pressure Sources Near an Airfoil Trailing Edge Under Separated Laminar Boundary Layers
Online Contents | 2011
|