Four-Bar Path Synthesis for Variable Camber Wing Using Two Steps Approach

Thumbnail Image

Date

2025-11-1

Authors

Journal Title

Journal ISSN

Volume Title

Publisher

Lecture notes in mechanical engineering

Abstract

Description

Keywords

Aeroelasticity and Vibration Control, Biomimetic flight and propulsion mechanisms, Model Reduction and Neural Networks

Citation

URI

https://dspace.kmitl.ac.th/handle/123456789/20189

Collections

All

Endorsement

Review

Supplemented By

Referenced By