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

Journal of Spacecraft and Rockets - United States
doi 10.2514/1.a32064
Full Text
Abstract

Available in full text

Date
Authors
Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Related search

Computational Techniques for Calculation of Missile Aerodynamic Coefficients

The International Conference on Electrical Engineering
2010English

Advances in Aerodynamic Shape Optimization

English

Multidisciplinary Aerodynamic-Structural Shape Optimization Using Deformation (MASSOUD)

2000English

Three-Dimensional Aerodynamic Shape Optimization Using Discrete Sensitivity Analysis

AIAA Journal
Aerospace Engineering
1996English

Aerodynamic Shape Optimization of Guided Missile Based on Wind Tunnel Testing and Computational Fluid Dynamics Simulation

Thermal Science
Renewable Energythe EnvironmentSustainability
2017English

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

1995English

A Method of Determining Some Aerodynamic Coefficients From Supersonic Free-Flight Tests of a Rolling Missile

Journal of the Aeronautical Sciences
1950English

Aerodynamic Shape Optimization Based on Free-Form Deformation

2004English

Viscous Aerodynamic Shape Optimization of Wings Including Planform Variables

2003English

Amanote Research

Note-taking for researchers

Follow Amanote

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

Privacy PolicyRefund Policy