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Fundamentals of aerodynamics / (Record no. 2052)

000 -LEADER
fixed length control field 01777cam a2200313 a 4500
003 - CONTROL NUMBER IDENTIFIER
control field OSt
005 - DATE AND TIME OF LATEST TRANSACTION
control field 20171004111108.0
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION
fixed length control field 091117s2011 nyua b 001 0 eng
020 ## - INTERNATIONAL STANDARD BOOK NUMBER
International Standard Book Number 9780071289085 (pbk.)
International Standard Book Number 0073398101
International Standard Book Number 9780073398105
International Standard Book Number 0071289089 (pbk.)
041 ## - Language
Language code of text/sound track or separate title eng
050 00 - LIBRARY OF CONGRESS CALL NUMBER
Classification number TL570
Item number .A677 2011
082 00 - DEWEY DECIMAL CLASSIFICATION NUMBER
Classification number 629.1323
Edition number 22
Item number A545
100 1# - MAIN ENTRY--PERSONAL NAME
Personal name Anderson, John David.
9 (RLIN) 3546
245 10 - IMMEDIATE SOURCE OF ACQUISITION NOTE
Title Fundamentals of aerodynamics /
Statement of responsibility, etc John D. Anderson, Jr.
250 ## - EDITION STATEMENT
Edition statement 5th ed.
260 ## - PUBLICATION, DISTRIBUTION, ETC. (IMPRINT)
Place of publication, distribution, etc New York :
Name of publisher, distributor, etc McGraw-Hill,
Date of publication, distribution, etc 2011.
300 ## - PHYSICAL DESCRIPTION
Extent xxiii, 1106 p. :
Other physical details ill. ;
Dimensions 24 cm.
440 #0 - SERIES STATEMENT/ADDED ENTRY--TITLE
Title Anderson series.
9 (RLIN) 13330
Title McGraw-Hill series in aeronautical and aerospace engineering.
9 (RLIN) 3549
504 ## - BIBLIOGRAPHY, ETC. NOTE
Bibliography, etc Includes bibliographical references (p. 1079-1084) and index.
505 0# - FORMATTED CONTENTS NOTE
Formatted contents note Aerodynamics -- Aerodynamics -- Fundamentals of inviscid, incompressible flow -- Incompressible flow over airfoils -- Incompressible flow over finite wings -- Three-dimensional incompressible flow -- Compressible flow -- Normal shock waves and related topics -- Oblique shock and expansion waves -- Compressible flow through nozzles, diffusers, and wind tunnels -- Subsonic compressible flow over airfoils -- Linearized supersonic flow -- Introduction to numerical techniques for nonlinear supersonic flow -- Elements of hypersonic flow -- Introduction to the fundamental principles and equations of viscous flow -- Special case -- Introduction to boundary layers -- Laminar boundary layers -- Turbulent boundary layers -- Navier-Stokes solutions.
650 #0 - SUBJECT ADDED ENTRY--TOPICAL TERM
Topical term or geographic name as entry element Aerodynamics.
9 (RLIN) 3547
800 1# - SERIES ADDED ENTRY--PERSONAL NAME
Personal name Anderson, John David.
Title of a work Anderson series.
9 (RLIN) 3548
830 #0 - SERIES ADDED ENTRY--UNIFORM TITLE
Uniform title McGraw-Hill series in aeronautical and aerospace engineering.
9 (RLIN) 3549
942 ## - ADDED ENTRY ELEMENTS (KOHA)
Source of classification or shelving scheme
Item type Book
Copies
Price effective from Permanent location Date last seen Not for loan Date acquired Source of classification or shelving scheme Koha item type Lost status Cost, normal purchase price Withdrawn status Source of acquisition Cost, replacement price Damaged status Barcode Shelving location Current location Public note Full call number
2011-09-05AUM Main Library2013-01-22 2013-01-22 Book 24.14 Jordan Book Centre 16.90 AUM-019598English Collections HallAUM Main LibraryJBC/2011/10770629.1323 A545
2011-09-05AUM Main Library2013-01-22 2013-01-22 Book 24.14 Jordan Book Centre 16.90 AUM-019599English Collections HallAUM Main LibraryJBC/2011/10770629.1323 A545
2011-09-05AUM Main Library2013-01-22 2013-01-22 Book 24.14 Jordan Book Centre 16.90 AUM-019600English Collections HallAUM Main LibraryJBC/2011/10770629.1323 A545
2011-09-05AUM Main Library2013-01-22 2013-01-22 Book 24.14 Jordan Book Centre 16.90 AUM-019601English Collections HallAUM Main LibraryJBC/2011/10770629.1323 A545