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Boundary-value problems for transonic flow

Author: A G Kuzʹmin
Publisher: Chichester : Wiley, ©2002.
Edition/Format:   eBook : Document : EnglishView all editions and formats
Database:WorldCat
Summary:
Transonic flow occurs around moving objects as they approach and cross the sound barrier. Serious problems can occur at this point, such as shock-induced flow separation which can cause the aircraft to spin out of control. Another important practical problem is the achievement of higher aerodynamic performance of aircraft at cruise conditions, which leads to considerable fuel savings. The success in application of  Read more...
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Genre/Form: Electronic books
Additional Physical Format: Print version:
Kuzʹmin, A.G. (Aleksandr Grigorʹevich).
Boundary-value problems for transonic flow.
Chichester : Wiley, ©2002
(OCoLC)49205791
Material Type: Document, Internet resource
Document Type: Internet Resource, Computer File
All Authors / Contributors: A G Kuzʹmin
ISBN: 047085295X 9780470852958
OCLC Number: 606840520
Reproduction Notes: Electronic reproduction. [S.l.] : HathiTrust Digital Library, 2010. MiAaHDL
Description: 1 online resource (xii, 304 pages) : illustrations
Details: Master and use copy. Digital master created according to Benchmark for Faithful Digital Reproductions of Monographs and Serials, Version 1. Digital Library Federation, December 2002.
Contents: Linear partial differential equations of mixed type --
Flow that accelerates from subsonic to supersonic velocity in a channel --
Flow with a local supersonic region --
Numerical simulation of transonic flow patterns --
Appendix A: Boundary-value problem with a damping condition.
Responsibility: Alexander G. Kuz'min.

Abstract:

Transonic flow occurs around moving objects as they approach and cross the sound barrier. Serious problems can occur at this point, such as shock-induced flow separation which can cause the aircraft to spin out of control. Another important practical problem is the achievement of higher aerodynamic performance of aircraft at cruise conditions, which leads to considerable fuel savings. The success in application of numerical methods for simulation of transonic flow and aircraft design depends on developments in the underlying mathematical theory.

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