AIAA-2019-3348: Flexibility Distribution Tuning by Wing Frame Inner Structure Morphing for Fixed-Wing Unmanned Aerial Vehicle
Multidiscplinary design optimization ; 2019 ; Dallas, TX
01.01.2019
12 pages
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Tail wing structure of fixed wing unmanned aerial vehicle
Europäisches Patentamt | 2015
|Morphing Wing Design for Fixed Wing Aircraft (AIAA 2015-0441)
British Library Conference Proceedings | 2015
|