All Stories

  1. Self-Aligned Focusing Schlieren at the 0.3-M Transonic Cryogenic Tunnel and the National Transonic Facility
  2. Model Preparation Areas for Propulsion Airframe Integration Testing at the NASA Langley Research Center
  3. A Discrete and Distributed Steady Blowing Application on a High Reynolds Number Semispan Supercritical Wing Configuration
  4. Transonic Drag Reduction Through Trailing-Edge Blowing on the FAST-MAC Circulation Control Model
  5. A Sweeping Jet Application on a High Reynolds Number Semi-Span Supercritical Wing Configuration
  6. Using Computational Fluid Dynamics and Experiments to Design Sweeping Jets for High Reynolds Number Cruise Configurations
  7. Femtosecond Laser Tagging Characterization of a Sweeping Jet Actuator Operating in the Compressible Regime
  8. Data Repeatability
  9. High Reynolds number flow quality
  10. Thrust Removal Methodology for the FAST-MAC Circulation Control Model Tested in the National Transonic Facility