Recent Development of Aerodynamic Design Methodologies

Inverse Design and Optimization
Softcover Nachdruck of the original 1. Auflage 1999
ISBN: 978-3-322-89954-5
Verlag: Vieweg+Teubner Verlag

Buch, Englisch, Band 65, 221 Seiten, Format (B × H): 155 mm x 235 mm, Gewicht: 365 g

Reihe: Notes on Numerical Fluid Mechanics

This volume contains an overview of the recent research in the field of "Aerodynamic Design Methodologies". Three categories of design methodologies are considered in this book: Genetic Algorithms, Inverse Design, and Optimization. Well-recognized researchers in the field cover each topic. Several methods, including a geometry parametrization method for airfoils and wings, are described in detail. Selected application examples demonstrate the large power and capabilities of these methods for the aerodynamic design of airfoils, wings, wing tips, control and high-lift devices, fuselages, wing-engine (with plume) arrangements, jet- engine compressors, turbines and blades.
The book is dedicated to the memory of Dr. Susumu Takanashi, who died in 1995 at the age of 56. He was a research scientist at the National Aerospace Laboratory, Japan and made enormous contributions to this field.

Zielgruppe

Research

Autoren/Hrsg.

Dulikravich, George

Fujii, Kozo

Fachgebiete

• Technische Wissenschaften Sonstige Technologien | Angewandte Technik Astronautik
• Naturwissenschaften Physik Mechanik
• Technische Wissenschaften Verkehrstechnik | Transportgewerbe Luft- und Raumfahrttechnik, Luftverkehr

Inhaltsverzeichnis

Multi Objective Aerodynamic Optimisation by Means of Robust and Efficient Genetic Algorithm.- Inverse Optimization Method for Aerodynamic Shape Design.- Subsonic Aerodynamic Design via Shape Optimization.- Parametric Airfoils and Wings.- Using Existing Flow-Field Analysis Codes for Inverse Design of Three-Dimensional Aerodynamic Shapes.- Numerical Methods for Inverse Solution in Aerodynamic Design of Turbomachinery.- Inverse Blade Design Based on Permeable Wall Concept.- An Inverse Design Method for Wings Using Integral Equaitons and Its Recent Progress.- Application of Transonic Inverse Method to the Development of Aerospace Products.- Aerodynamic Design of Wing-Engine Configuration under Effect of Jet Plume.