Inverse aerodynamic design applications using the MGM hybrid formulation

Autor:	Guilherme Lara Oliveira, Luis C.C. Santos, Marcelo Hayashi, Ernani Volpe, Marco Ceze
Rok vydání:	2009
Předmět:	Engineering Mathematical optimization business.industry Applied Mathematics General Engineering Inverse Aerodynamics Computational fluid dynamics Computer Science Applications Swept wing Aerospace engineering business Aerospace Inverse method Fourier series Transonic
Zdroj:	Inverse Problems in Science and Engineering. 17:245-261
ISSN:	1741-5985 1741-5977
DOI:	10.1080/17415970802083615
Popis:	The well-known modified Garabedian–Mcfadden (MGM) method is an attractive alternative for aerodynamic inverse design, for its simplicity and effectiveness (P. Garabedian and G. Mcfadden, Design of supercritical swept wings, AIAA J. 20(3) (1982), 289–291; J.B. Malone, J. Vadyak, and L.N. Sankar, Inverse aerodynamic design method for aircraft components, J. Aircraft 24(2) (1987), 8–9; Santos, A hybrid optimization method for aerodynamic design of lifting surfaces, PhD Thesis, Georgia Institute of Technology, 1993). Owing to these characteristics, the method has been the subject of several authors over the years (G.S. Dulikravich and D.P. Baker, Aerodynamic shape inverse design using a Fourier series method, in AIAA paper 99-0185, AIAA Aerospace Sciences Meeting, Reno, NV, January 1999; D.H. Silva and L.N. Sankar, An inverse method for the design of transonic wings, in 1992 Aerospace Design Conference, No. 92-1025 in proceedings, AIAA, Irvine, CA, February 1992, 1–11; W. Bartelheimer, An Improved Integral Eq...
Databáze:	OpenAIRE
Externí odkaz:	https://explore.openaire.eu/search/publication?articleId=doi_________::dcdf4d179c2a0b70e80a3215faea8c67 https://doi.org/10.1080/17415970802083615 Zobrazit plný text záznamu Plný text ve formátu PDF Plný text ve formátu HTML
Nepřihlášeným uživatelům se plný text nezobrazuje	K zobrazení výsledku je třeba se přihlásit.