000 -LEADER |
fixed length control field |
01734cam a2200229 a 4500 |
001 - CONTROL NUMBER |
control field |
vtls003026272 |
003 - CONTROL NUMBER IDENTIFIER |
control field |
MY-SjTCS |
005 - DATE AND TIME OF LATEST TRANSACTION |
control field |
20200306155026.0 |
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION |
fixed length control field |
110218s2005 enkaf b 001 0 eng |
020 ## - INTERNATIONAL STANDARD BOOK NUMBER |
International Standard Book Number |
0470855401 (hbk.) |
039 #9 - LEVEL OF BIBLIOGRAPHIC CONTROL AND CODING DETAIL [OBSOLETE] |
Level of rules in bibliographic description |
201102181353 |
Level of effort used to assign nonsubject heading access points |
VLOAD |
Level of effort used to assign subject headings |
200605051425 |
Level of effort used to assign classification |
eunice |
Level of effort used to assign subject headings |
200603081226 |
Level of effort used to assign classification |
meena |
-- |
200602221603 |
-- |
meena |
082 04 - DEWEY DECIMAL CLASSIFICATION NUMBER |
Classification number |
629.10285 |
Item number |
KEA |
100 1# - MAIN ENTRY--PERSONAL NAME |
Personal name |
Keane, A. J. |
9 (RLIN) |
220463 |
245 10 - TITLE STATEMENT |
Title |
Computational approaches for aerospace design : |
Remainder of title |
the pursuit of excellence / |
Statement of responsibility, etc. |
Andy J. Keane, Prasanth B. Nair. |
260 ## - PUBLICATION, DISTRIBUTION, ETC. |
Place of publication, distribution, etc. |
Chichester, England : |
Name of publisher, distributor, etc. |
John Wiley, |
Date of publication, distribution, etc. |
c2005. |
300 ## - PHYSICAL DESCRIPTION |
Extent |
xx, 582 p., [4] p. of plates : |
Other physical details |
ill. (some col.) ; |
Dimensions |
25 cm. |
505 0# - FORMATTED CONTENTS NOTE |
Formatted contents note |
Foreword. - Preface. - Acknowledgment. - 1. Preliminaries. 1. Introduction. - 2. Design-oriented analysis. 3. Elements of numerical optimization. - II. Sensitivity analysis and approximation concepts. 4. Sensitivity analysis. 5. General approximation concepts and surrogates. 6. Physics-based approximations. - III. Frameworks for design space exploration. 7. Managing surrogate models in optimization. 8. Design in the presence of uncertainty. 9. Architectures for multidisciplinary optimization. - IV. Case studies. 10. A problem in satellite design. 11. Airfoil section design. 12. Aircraft wing design - data fusion between codes. 13. Turbine blade design (1) - guide-vane SKE control. 14. Turbine blade design (II) - Fir-tree root geometry. 15. Aero-engine nacelle design using the geodise toolkit. 16. Getting the optimization process started. - Bibliography. - Index. |
650 #0 - SUBJECT ADDED ENTRY--TOPICAL TERM |
Topical term or geographic name entry element |
Aerospace engineering |
General subdivision |
Data processing. |
9 (RLIN) |
220464 |
650 #0 - SUBJECT ADDED ENTRY--TOPICAL TERM |
Topical term or geographic name entry element |
Aerospace engineering |
General subdivision |
Mathematics. |
9 (RLIN) |
220465 |
700 1# - ADDED ENTRY--PERSONAL NAME |
Personal name |
Nair, P. B. |
Relator term |
(j.a.) |
9 (RLIN) |
220466 |
920 ## - Programme |
Programme |
GEN : 32179 |
999 ## - SYSTEM CONTROL NUMBERS (KOHA) |
Koha biblionumber |
35620 |
Koha biblioitemnumber |
35620 |