Shock wave-boundary-layer interactions / (Record no. 6351)

MARC details
000 -LEADER
fixed length control field 03524cam a22003974a 4500
001 - CONTROL NUMBER
control field 16611752
003 - CONTROL NUMBER IDENTIFIER
control field OSt
005 - DATE AND TIME OF LATEST TRANSACTION
control field 20210930200225.0
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION
fixed length control field 110114s2011 enka b 001 0 eng
010 ## - LIBRARY OF CONGRESS CONTROL NUMBER
LC control number 2011001978
016 7# - NATIONAL BIBLIOGRAPHIC AGENCY CONTROL NUMBER
Record control number 015794418
Source Uk
020 ## - INTERNATIONAL STANDARD BOOK NUMBER
International Standard Book Number 9780521848527 (hardback)
020 ## - INTERNATIONAL STANDARD BOOK NUMBER
International Standard Book Number 0521848520 (hardback)
035 ## - SYSTEM CONTROL NUMBER
System control number (OCoLC)ocn701672464
040 ## - CATALOGING SOURCE
Original cataloging agency DLC
Transcribing agency DLC
Modifying agency YDX
-- YDXCP
-- UKMGB
-- CDX
-- DLC
042 ## - AUTHENTICATION CODE
Authentication code pcc
050 00 - LIBRARY OF CONGRESS CALL NUMBER
Classification number TL574.S4
Item number S575 2011
082 00 - DEWEY DECIMAL CLASSIFICATION NUMBER
Classification number 629.132/37
Edition number 22
084 ## - OTHER CLASSIFICATION NUMBER
Classification number TEC009000
Number source bisacsh
245 00 - TITLE STATEMENT
Title Shock wave-boundary-layer interactions /
Statement of responsibility, etc. edited by Holger Babinsky, John K. Harvey.
260 ## - PUBLICATION, DISTRIBUTION, ETC.
Place of publication, distribution, etc. Cambridge ;
-- New York :
Name of publisher, distributor, etc. Cambridge University Press,
Date of publication, distribution, etc. 2011.
300 ## - PHYSICAL DESCRIPTION
Extent xvii, 461 p. :
Other physical details ill. ;
Dimensions 26 cm.
490 1# - SERIES STATEMENT
Series statement Cambridge aerospace series
504 ## - BIBLIOGRAPHY, ETC. NOTE
Bibliography, etc. note Includes bibliographical references and index.
505 8# - FORMATTED CONTENTS NOTE
Formatted contents note Machine generated contents note: 1. Introduction John K. Harvey and Holger Babinsky; 2. Physical introduction Jean Delery; 3. Transonic shock wave boundary layer interactions Holger Babinsky and Jean Delery; 4. Ideal gas shock wave turbulent boundary layer interactions in supersonic flows and their modeling -- two dimensional interactions Alexander A. Zheltovodov and Doyle D. Knight; 5. Ideal gas shock wave turbulent boundary layer interactions in supersonic flows and their modeling -- three dimensional interactions Doyle D. Knight and Alexander A. Zheltovodov; 6. Experimental studies of shock wave/boundary layer interactions in hypersonic flows Michael S. Holden; 7. Numerical simulation of hypersonic shock wave boundary layer interactions Graham V. Candler; 8. Shock wave/boundary layer interactions taking place in hypersonic flows John K. Harvey; 9. Shock wave unsteadiness in turbulent shock wave boundary layer interactions P. Dupont, J.F Debieve, and J.P Dussauge; 10. Analytical treatment of shock/boundary layer interactions George Inger.
520 ## - SUMMARY, ETC.
Summary, etc. "This is the first book devoted solely to the phenomenon of Shock Wave Boundary Layer Interactions and covers all flow regimes where SBLI's occur"--Provided by publisher.
520 ## - SUMMARY, ETC.
Summary, etc. "Shock Wave/Boundary Layer Interaction (SBLI) is a fundamental phenomenon in gas dynamics and frequently a defining feature in high speed aerodynamic flowfields. The interactions can be found in practical situations, ranging from transonic aircraft wings to hypersonic vehicles and engines. SBLI's have the potential to pose serious problems and is thus a critical issue for aerospace applications. This is the first book devoted solely to a comprehensive, state of the art explanation of the phenomenon with coverage of all flow regimes where SBLI's occur. The book includes contributions from leading international experts who share their insight into SBLI physics and the impact of these interactions on practical flow situations. This book is aimed at practitioners and graduate students in aerodynamics who wish to familiarise themselves with all aspects of SBLI flows. It is a valuable resource for the specialist because it gathers experimental, computational and theoretical knowledge in one place"--Provided by publisher.
650 #0 - SUBJECT ADDED ENTRY--TOPICAL TERM
Topical term or geographic name entry element Shock waves.
650 #0 - SUBJECT ADDED ENTRY--TOPICAL TERM
Topical term or geographic name entry element Boundary layer.
700 1# - ADDED ENTRY--PERSONAL NAME
Personal name Babinsky, Holger.
700 1# - ADDED ENTRY--PERSONAL NAME
Personal name Harvey, John
Fuller form of name (John K.)
830 #0 - SERIES ADDED ENTRY--UNIFORM TITLE
Uniform title Cambridge aerospace series.
906 ## - LOCAL DATA ELEMENT F, LDF (RLIN)
a 7
b cbc
c orignew
d 1
e ecip
f 20
g y-gencatlg
942 ## - ADDED ENTRY ELEMENTS (KOHA)
Source of classification or shelving scheme Library of Congress Classification
Koha item type Books
Holdings
Withdrawn status Lost status Source of classification or shelving scheme Damaged status Not for loan Home library Current library Shelving location Date acquired Total Checkouts Full call number Barcode Date last seen Price effective from Koha item type
    Library of Congress Classification     Kwara State University Library Kwara State University Library   2018-07-13   TL574.S4557 2011-01 013836-01 2018-07-13 2018-07-13 Books
    Library of Congress Classification     Kwara State University Library Kwara State University Library   2018-07-13   TL574.S4557 2011-01 013836-02 2018-07-13 2018-07-13 Books