Aerodynamic Optimization of a UAV Wing Subject to Weight, Geometric, Root Bending Moment, and Performance Constraints

International Journal of Aerospace Engineering - Egypt
doi 10.1155/2019/3050824
Full Text
Abstract

Available in full text

Date
Authors
Publisher

Hindawi Limited

Related search

Aerodynamic Design Considerations of a Flying Wing Type Uav

SCIENTIFIC RESEARCH AND EDUCATION IN THE AIR FORCE
2017English

Multimodality in Aerodynamic Wing Design Optimization

AIAA Journal
Aerospace Engineering
2019English

Aerodynamic Shape Optimization of Wing and Wing-Body Configurations Using Control Theory

1995English

Aerodynamic Design Optimization Studies of a Blended-Wing-Body Aircraft

Journal of Aircraft
Aerospace Engineering
2014English

Wing Aerodynamic Optimization by Using Genetic Algoritm and Ansys

Acta Physica Polonica A
AstronomyPhysics
2017English

Optimization of the Aerodynamic Performance of Regional and Wide-Body-Class Blended Wing-Body Aircraft

2015English

Numerical Analysis and Estimation of Aerodynamic Performance of a Geometric Twisted Wing Configuration Using NACA 23012, NACA 23015 and NACA 23018

International Journal for Research in Applied Science and Engineering Technology
2020English

MDO Architectures for Coupled Aerodynamic and Structural Optimization of a Flexible Wing

2004English

RANS-based Aerodynamic Shape Optimization of a Blended-Wing-Body Aircraft

2013English

Amanote Research

Note-taking for researchers

Follow Amanote

© 2025 Amaplex Software S.P.R.L. All rights reserved.

Privacy PolicyRefund Policy