All Stories

  1. Aerodynamic and structural design of winglet with integrated VHF antenna
  2. Improvement of Computational Results of NASA Airliner Model by Wing Modal Analysis
  3. Active Flow Separation Control Applied at Wing-Pylon Junction of a Wing Section in Landing Configuration
  4. Improvement of CFD results of NASA CRM by on-line mesh deformation using modal analysis of a wing
  5. Response Surface Method Application to High-Lift Configuration with Active Flow Control