Airfoil Shape Design and Optimization Using Multifidelity Analysis and Embedded Inverse Design

AIAA Journal - United States
doi 10.2514/1.18766
Full Text
Abstract

Available in full text

Date
Authors
Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Related search

An Inverse Approach for Airfoil Design

2008English

Inverse Airfoil Design Utilizing CST Parameterization

2010English

A Multifidelity Gradient-Free Optimization Method and Application to Aerodynamic Design

2008English

An Efficient Low-Speed Airfoil Design Optimization Process Using Multi-Fidelity Analysis for UAV Flying Wing

2016English

Design of a New Urban Wind Turbine Airfoil Using a Pressure-Load Inverse Method

Renewable Energy
Renewable Energythe EnvironmentSustainability
2009English

Transonic Airfoil Design and Optimization for an Unmanned Air Vehicle Concept

Journal of Mechanics Engineering and Automation
2019English

Structure and Appearance Optimization for Controllable Shape Design

ACM Transactions on Graphics
Computer GraphicsComputer-Aided Design
2015English

Shape Design Optimization of Hyperelastic Structures Using a Meshless Method

AIAA Journal
Aerospace Engineering
1999English

Low-Speed Natural-Laminar-Flow Airfoils: Case Study in Inverse Airfoil Design

Journal of Aircraft
Aerospace Engineering
2001English

Amanote Research

Note-taking for researchers

Follow Amanote

© 2026 Amaplex Software S.P.R.L. All rights reserved.

Privacy PolicyRefund Policy