Flutter Analysis of Mission-Adaptive Wing with Variable Camber Continuous Trailing Edge Flap (AIAA 2014-0839)
Conference; 55th, AIAA/ASME/ASME/ASCE/AHS/SC Structures, structural dynamics and materials ; 2014 ; National Harbor, MD
01.01.2014
39 pages
Includes bibliographical references and author index
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
British Library Conference Proceedings | 2014
|British Library Conference Proceedings | 2015
|SAE Technical Papers | 2015
|British Library Conference Proceedings | 2014
|