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Aeroservoelastic wind-tunnel investigations using the active flexible wing model - Status and recent accomplishments
1989
30th Structures, Structural Dynamics and Materials Conference
unpublished
This paper describes the status of the joint NASA/ Rockwell Active Flexible Wing Wind-Tunnel Test Program. The objectives of the program are to develop and validate the analysis, design and test methodologies required toapply multifunction active control technology for improv-21. No. of pages 22. Price
doi:10.2514/6.1989-1168
fatcat:geep22qmbbajlmoejzy7z4dn3e