Transonic aerodynamics : problems in asymptotic theory /

Saved in:
Bibliographic Details
Imprint:Philadelphia, Pa. : Society for Industrial and Applied Mathematics (SIAM, 3600 Market Street, Floor 6, Philadelphia, PA 19104), 1993.
Description:1 online resource (x, 90 pages) : illustrations, digital file
Language:English
Series:Frontiers in applied mathematics ; 12
Frontiers in applied mathematics ; 12.
Subject:
Format: E-Resource Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/12577440
Hidden Bibliographic Details
Other authors / contributors:Cook, L. Pamela.
Society for Industrial and Applied Mathematics.
International Conference on Industrial and Applied Mathematics (2nd : 1991 : Washington, D.C.)
ISBN:9781611970975
1611970970
0898713102
9780898713107
Notes:Title from title screen, viewed 04/05/2011.
"Originated from a minisymposium organized by the editor at the second ICIAM meeting (International Conference on Industrial and Applied Mathematics) in Washington, D.C., July 1991"--Preface.
Includes bibliographical references and index.
Restricted to subscribers or individual electronic text purchasers.
Also available in print version.
English.
Summary:This volume offers exciting results, perspectives, and case studies for the treatment of problems arising in transonic aerodynamics. New advances including triple deck theory, analysis of stagnation at the nose of a body, transonic choked flow, and the transonic area rule are presented. Interest in analyzing the transonic range of flight, its stability properties, and especially the question of designing reduced drag (shockless or weak shock) airfoils keeps growing. Present day commercial aircraft cruise in the transonic range. Mechanical and aeronautical engineers interested in compressible fluid flows, design of optimal wings, and an understanding of transonic flow held about wings and airfoils will find the book invaluable. This book is understandable to those with a knowledge of continuum mechanics (fluids) and asymptotic methods. It is appropriate for graduate courses in aerodynamics and mathematical methods.
Other form:Print version: 0898713102 9780898713107