Computational Evaluation of a Damage Assessment Model for UAV Wings
AIAA SCITECH 2023 Forum
2023-01-01
Conference paper
Electronic Resource
English
Structural damage assessment of MAV flapping wings using DIC-wavelet technique
British Library Conference Proceedings | 2020
|Computational model of flexible membrane wings in steady laminar flow
Tema Archive | 1995
|Computational Model of Flexible Membrane Wings in Steady Laminar Flow
Online Contents | 1995
|Computational Investigation of Flow Control over Wings
AIAA | 2007
|