The Aeromechanics Branch of the Flight Vehicle Research and Technolory Division is responsible for aeromechanics research activities that directly support the civil competiveness of the U.S. helicopter industry and the Department of Defense. Branch programs address all aspects of the rotorcraft which directly influence the vehicle's performance, structural, and dynamic response, external acoustics, vibration, and aeroelastic stability. The programs are both theoretical and experimental in nature.

Advanced computational methodology research using computational fluid dynamics and multidisciplinary comprehensive analyses seeks to understand the complete rotorcraft's operating environment and to develop analytical models to predict rotorcraftaerodynamic, aeroacoustic, and dynamic behavior. Experimental research seeks to obtain accurate data to validate these analyses, investigate phenomena currently beyond predictive capability, and to achieve rapid solutions to flight vehicle problems. Databases from the flight and wind tunnel experimental programs are validated, documented and maintained for the benefit of the U.S. rotorcraft technology base.

The Branch directly supports the Aeronautics Research Mission Directorate at NASA Headquarters under the Fundamental Aeronautics Program and the Subsonic Rotary Wing Project in particular.

NASA Ames Research Center, Moffett Field CA 94035-1000, (650) 604-5000
URL: http://rotorcraft.arc.nasa.gov/
This Website Maintained By: Randall L. Peterson.
Responsible NASA Official: Dr. William Warmbrodt (Chief)

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Last Modified: Monday, 20-Apr-2009 10:08:13 PDT