On the Design and Aeroelastic Stability Analysis of Twin Wing-Tail Boom Configuration Unmanned Air Vehicle
Conference; 52nd, AIAA/ASME/ASME/ASCE/AHS/ASC Structures, structural dynamics and materials ; 2011 ; Denver, CO
2011-01-01
42 pages
Includes bibliographical references and author index
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Tail boom hanger of fixed-wing unmanned aerial vehicle
Europäisches Patentamt | 2020
|Double-tail-boom tail folding mechanism of unmanned aerial vehicle
Europäisches Patentamt | 2022
|