All Stories

  1. Shock-Wave/Boundary-Layer Interaction in a Large-Aspect-Ratio Test Section
  2. Reynolds-Averaged Navier-Stokes Technology for Transonic Drag Prediction: A Boeing Perspective
  3. Numerical Investigation of a Normal Shock Wave Boundary Layer Interaction in a 4.3 Aspect Ratio Test Section
  4. Computational and Experimental Results for Flows in a Diffusing S-Duct without and with Flow Control Devices