Accession Number : ADA388195


Title :   Structural Aspects of Flexible Aircraft Control (les Aspects structuraux du controle actif et flexible des aeronefs)


Descriptive Note : Proceedings,


Corporate Author : NATO RESEARCH AND TECHNOLOGY ORGANIZATION NEUILLY-SUR-SEINE (FRANCE)


Full Text : https://apps.dtic.mil/dtic/tr/fulltext/u2/a388195.pdf


Report Date : May 2000


Pagination or Media Count : 289


Abstract : The Specialists' Meeting dealt with Design Issues and more specifically Structural Aspects of Flexible Aircraft Control. Twenty six papers and a Keynote address were presented with the following objective: How the design methods used in the development of military fighter aircraft can be improved, and applied to transport aircraft design applications. There were three sessions covering the following topics: 1. Aeroservoelasticity 2. Active Control of Flexible Structure I 2. Active Control of Flexible Structure II


Descriptors :   *STRUCTURAL ENGINEERING , *AIRCRAFT DESIGN , MATHEMATICAL MODELS , NATO , FIGHTER AIRCRAFT , INTEGRATED SYSTEMS , MILITARY AIRCRAFT , STRUCTURAL PROPERTIES , STATIC LOADS , AEROELASTICITY , FRANCE , TRANSPORT AIRCRAFT , SERVOMECHANISMS , FLUTTER , FLEXIBLE STRUCTURES


Subject Categories : Aerodynamics
      Aircraft
      Structural Engineering and Building Technology


Distribution Statement : APPROVED FOR PUBLIC RELEASE