Computatianal methods for the aerodynamic design of aircraft componenets英文电子书.pdf

Annual Reviews /aronline Annu. Rev. Fluid Mech. 1993.25:183-214 Copyright © 1993 by Annual Reviews Inc. All rights reserved COMPUTATIONAL METHODS FOR THE AERODYNAMIC g r o . s DESIGN OF AIRCRAFT w e i v e r COMPONENTS l a u n n a . s l Th. E. Labrujdre and J. W. Slooff a n . r y u l n o o j Aerodynamics Division, National Aerospace Laboratory NLR, r a e s m u A. Fokkerweg 2, 1059 CM Amsterdam, The Netherlands o l r a f n d o s e r d e KEY WORDS: inverse design, optimal control, multi-point design, design con- a p o r l o straints n F w o 8. D 0 / 4. 6 1 2 2 / INTRODUCTION 5 - 0 3 8 n 1 o : 5 2 The present article reviews state-of-the-art computational aerodynamic 2 i . L 3 S design methods. The review is limited to methods aimed directly at the 9 E 9 N 1 . y determination of geometries for which certain specified aerodynamic prop- h b c erties can be obtained, with or without constraints on the geometry. Cut- e M d and-try methodologies, which utilize analysis methods only, are not con- i u l sidered. The review is further limited to methods which are considered F . v representative of different approaches and to methods illustrating the e R . latest developments. Also, a