First-In-Flight Full-Scale Application of Active Flow Control: The XV-15 Tiltrotor Download Reduction

Abstract

In June 2003, before being retired to the Smithsonian Museum Annex, near Dulles Airport, the only remaining XV-15 tiltrotor aircraft was used for a series of flight tests to demonstrate the effectiveness of Active flow Control (AFC) in reducing the download during hover. The flaps/ailerons were retrofitted with actuators delivering zero-mass-flux periodic jets emanating from slots positioned tangential to the surface. The flight tests followed two extensive sets of model experiments, and the program included participation form University of Arizona, Illinois Institute of Technology, Tel Aviv University, Bell Helicopter and Boeing under the sponsorship of the Micro-Adaptive Flow control (MAFC) program of DARPA. The over six hours of flight tests successfully achieved the two goals and documented reduction in the download forces by 9 to 14%, thereby demonstrating for the first time the aerodynamic principals of AFC extend to full-scale flight.

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Document Details

Document Type
Technical Report
Publication Date
Oct 01, 2004
Accession Number
ADA442393

Entities

People

  • Aaron D. Stalker
  • Hassan M. Nagib
  • Israel J. Wygnanski
  • John W. Kiedaisch
  • Michael A. Mcveigh
  • Tom Wood

Organizations

  • Illinois Institute of Technology

Tags

Communities of Interest

  • Air Platforms
  • Biomedical
  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Aircraft Equipment
  • Aircrafts
  • Airframes
  • Boundary Layer
  • Computational Fluid Dynamics
  • Flow
  • Flow Visualization
  • Fluid Dynamics
  • Fluid Flow
  • High Lift Devices
  • Hypervelocity Flow
  • Pressure Distribution
  • Pressure Measurement
  • Tilt Rotor Aircraft
  • Turbulent Mixing
  • Two Dimensional
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Aviation Safety and Air Traffic Management
  • Database Systems and Applications
  • Technical Research and Report Writing.