NavAIR Hleicopter/Frigate Airwake Interaction

Grants

Abstract

  • Development of a wind tunnel methodology to identify areas of aerodynamic coupling of helicopter downwash and frigate airwake. PIV measurements usign a simplified rotor and frigate model.
  • Date/time Interval

  • 2010 - 2011
  • Awarded By

    Total Award Amount

  • $17,200.00
  • Contributor

  • Drew Landman   Investigator  
  • Drew Landman   Investigator