Active Flexible Wing model mounted in the Langley TDT
The Active Flexible Wing (AFW) program was initially a joint U.S. Air Force, NASA and Rockwell International effort to demonstrate the AFW concept. The AFW concept involves achieving vehicle weight savings through advantageous use of a flexible wing surface via active control applications. Under this initial program, two wind-tunnel tests were completed in the Langley TDT. A second AFW model program was undertaken by NASA and Rockwell Inter-national with the goal of demonstrating aeroelastic control through the use of digital active control technology. The multiple-exposure photograph shows the AFW model at several pitch positions during a TDT entry under this follow-on program. Key accomplishments of this second program included single and multiple- mode flutter suppression, load alleviation and load control during rapid roll maneuvers, and multi-input/multi-output multiple function active controls tests above the open loop flutter boundary.
NASA Identifier: L91-2130
Date Taken: |
09.23.2009 |
Date Posted: |
10.10.2012 16:30 |
Photo ID: |
708845 |
Resolution: |
1536x1348 |
Size: |
295.44 KB |
Location: |
WASHINGTON, DC, US |
Web Views: |
37 |
Downloads: |
1 |
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