| 000 -LEADER |
|---|
| fixed length control field |
03379cam a2200397 i 4500 |
| 001 - CONTROL NUMBER |
|---|
| control field |
17813863 |
| 005 - DATE AND TIME OF LATEST TRANSACTION |
|---|
| control field |
20230324093830.0 |
| 008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION |
|---|
| fixed length control field |
130716s2014 flu b 001 0 eng |
| 010 ## - LIBRARY OF CONGRESS CONTROL NUMBER |
|---|
| LC control number |
2013027555 |
| 020 ## - INTERNATIONAL STANDARD BOOK NUMBER |
|---|
| International Standard Book Number |
9781439886021 (hardback : acidfree paper) |
| 040 ## - CATALOGING SOURCE |
|---|
| Original cataloging agency |
DLC |
| Language of cataloging |
eng |
| Transcribing agency |
DLC |
| Description conventions |
rda |
| Modifying agency |
DLC |
| 042 ## - AUTHENTICATION CODE |
|---|
| Authentication code |
pcc |
| 050 00 - LIBRARY OF CONGRESS CALL NUMBER |
|---|
| Classification number |
TL570 |
| Item number |
.S53 2014 |
| 082 00 - DEWEY DECIMAL CLASSIFICATION NUMBER |
|---|
| Classification number |
629.1323 |
| Edition number |
23 |
| Author Mark |
SIN |
| 084 ## - OTHER CLASSIFICATION NUMBER |
|---|
| Classification number |
SCI041000 |
| -- |
TEC007000 |
| -- |
TEC009070 |
| Number source |
bisacsh |
| 100 1# - MAIN ENTRY--PERSONAL NAME |
|---|
| Personal name |
Sinha, Nandan K. |
| 9 (RLIN) |
110542 |
| 245 10 - TITLE STATEMENT |
|---|
| Title |
Elementary flight dynamics with an introduction to bifurcation and continuation methods / |
| Statement of responsibility, etc. |
Nandan K. Sinha, N. Ananthkrishnan. |
| 264 #1 - PRODUCTION, PUBLICATION, DISTRIBUTION, MANUFACTURE, AND COPYRIGHT NOTICE |
|---|
| Place of production, publication, distribution, manufacture |
Boca Raton : |
| Name of producer, publisher, distributor, manufacturer |
CRC Press, Taylor & Francis Group, CRC Press is an imprint of the Taylor & Francis Group, an informa business, |
| Date of production, publication, distribution, manufacture, or copyright notice |
[2014] |
| 300 ## - PHYSICAL DESCRIPTION |
|---|
| Extent |
xvii, 354 pages ; |
| Dimensions |
25 cm |
| 336 ## - CONTENT TYPE |
|---|
| Content type term |
text |
| Source |
rdacontent |
| 337 ## - MEDIA TYPE |
|---|
| Media type term |
unmediated |
| Source |
rdamedia |
| 338 ## - CARRIER TYPE |
|---|
| Carrier type term |
volume |
| Source |
rdacarrier |
| 504 ## - BIBLIOGRAPHY, ETC. NOTE |
|---|
| Bibliography, etc. note |
Includes bibliographical references (page 340) and index. |
| 520 ## - SUMMARY, ETC. |
|---|
| Summary, etc. |
"Preface Flight mechanics lies at the heart of aeronautics. It is the point of confluence of other disciplines within aerospace engineering and the gateway to aircraft design. Almost every curriculum in aerospace engineering includes two courses in flight mechanics--one on applied aerodynamics and airplane performance and the other on airplane stability/control and flight dynamics. Having taught both these subjects for over two decades, the authors' experience can be summed up briefly in the following student response: 'These are the best subjects in the curriculum. When you teach it in class, everything is obvious, but when we go back and read the textbook, things get very confusing'. As we got down to decoding this statement, several questions emerged: - Why put students through the gruesome derivation of the sixdegree- of-freedom equations early in the course, preceded by the axis transformations, and followed by the small perturbation math, when the bulk of the course is focussed on the dynamic modes about straight and level flight trim, which can be easily presented without going this route? - Would it not be nicer to write the equations for the second-order modes in a manner similar to a spring-mass-damper system? Then, one could read off the stiffness and damping directly, which would also give the conditions for stability. - The definitions of 'static' and 'dynamic' stability have been the cause of much student heartbreak. With the second-order form of the equations, the requirement of positive stiffness is the same as the socalled 'static' stability condition, so why not drop the separate notion of static stability entirely? -"-- |
| Assigning source |
Provided by publisher. |
| 650 #0 - SUBJECT ADDED ENTRY--TOPICAL TERM |
|---|
| Topical term or geographic name entry element |
Aerodynamics. |
| 9 (RLIN) |
2589 |
| 650 #0 - SUBJECT ADDED ENTRY--TOPICAL TERM |
|---|
| Topical term or geographic name entry element |
Bifurcation theory. |
| 9 (RLIN) |
10650 |
| 650 #0 - SUBJECT ADDED ENTRY--TOPICAL TERM |
|---|
| Topical term or geographic name entry element |
Continuation methods. |
| 9 (RLIN) |
39881 |
| 650 #7 - SUBJECT ADDED ENTRY--TOPICAL TERM |
|---|
| Topical term or geographic name entry element |
SCIENCE / Mechanics / General. |
| Source of heading or term |
bisacsh |
| 650 #7 - SUBJECT ADDED ENTRY--TOPICAL TERM |
|---|
| Topical term or geographic name entry element |
TECHNOLOGY & ENGINEERING / Electrical. |
| Source of heading or term |
bisacsh |
| 650 #7 - SUBJECT ADDED ENTRY--TOPICAL TERM |
|---|
| Topical term or geographic name entry element |
TECHNOLOGY & ENGINEERING / Mechanical. |
| Source of heading or term |
bisacsh |
| 700 1# - ADDED ENTRY--PERSONAL NAME |
|---|
| Personal name |
Ananthkrishnan, N. |
| 9 (RLIN) |
110543 |
| 856 42 - ELECTRONIC LOCATION AND ACCESS |
|---|
| Materials specified |
Cover image |
| Uniform Resource Identifier |
<a href="http://images.tandf.co.uk/common/jackets/websmall/978143988/9781439886021.jpg">http://images.tandf.co.uk/common/jackets/websmall/978143988/9781439886021.jpg</a> |
| 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 |
|
| Koha item type |
Book |
