Computing Stability Derivatives and Their Gradients for Aerodynamic Shape Optimization

AIAA Journal - United States
doi 10.2514/1.j052922
Full Text
Abstract

Available in full text

Date
Authors
Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Related search

Advances in Aerodynamic Shape Optimization

English

Multidisciplinary Aerodynamic-Structural Shape Optimization Using Deformation (MASSOUD)

2000English

Aerodynamic Shape Optimization Based on Free-Form Deformation

2004English

Output Error Estimates and Mesh Refinement in Aerodynamic Shape Optimization

2013English

Three-Dimensional Aerodynamic Shape Optimization Using Discrete Sensitivity Analysis

AIAA Journal
Aerospace Engineering
1996English

Viscous Aerodynamic Shape Optimization of Wings Including Planform Variables

2003English

Aerodynamic Shape Optimization System of a Canard-Controlled Missile Using Trajectory-Dependent Aerodynamic Coefficients

Journal of Spacecraft and Rockets
SpacePlanetary ScienceAerospace Engineering
2012English

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

1995English

Aerodynamic Shape Optimization of Common Research Model Wing–Body–Tail Configuration

Journal of Aircraft
Aerospace Engineering
2016English

Amanote Research

Note-taking for researchers

Follow Amanote

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

Privacy PolicyRefund Policy