Aircraft performance / (Record no. 2391)
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| 000 -LEADER | |
|---|---|
| fixed length control field | 02268nam a2200169 a 4500 |
| 001 - CONTROL NUMBER | |
| control field | ASIN0470044160 |
| 005 - DATE AND TIME OF LATEST TRANSACTION | |
| control field | 20190522115059.0 |
| 008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION | |
| fixed length control field | 120502s2006 xxu eng d |
| 020 ## - INTERNATIONAL STANDARD BOOK NUMBER | |
| International Standard Book Number | 0470044160 (hardcover) |
| Terms of availability | $140.00 |
| 020 ## - INTERNATIONAL STANDARD BOOK NUMBER | |
| International Standard Book Number | 9780470044162 (hardcover) |
| 100 1# - MAIN ENTRY--PERSONAL NAME | |
| Personal name | Saarlas, Maido. |
| 245 10 - TITLE STATEMENT | |
| Title | Aircraft performance / |
| Statement of responsibility, etc. | Maido Saarlas. |
| 260 ## - PUBLICATION, DISTRIBUTION, ETC. | |
| Place of publication, distribution, etc. | [S.l.] : |
| Name of publisher, distributor, etc. | Wiley, |
| Date of publication, distribution, etc. | 2006. |
| 300 ## - PHYSICAL DESCRIPTION | |
| Extent | 296 p. ; |
| Dimensions | 24 cm. |
| 520 ## - SUMMARY, ETC. | |
| Summary, etc. | Straightforward methods to design and operate aircraft to meet performance specifications Aircraft Performance sets forth a group of tested and proven methods needed to determine the performance of an aircraft. The central theme of this book is the energy method, which enhances understanding of the standard methods and provides accessibility to advanced topics. As a result, readers gain a thorough understanding of the performance issues involved in operating an aircraft in an efficient and economic manner. While covering all the standard topics--level and climbing flight, range and endurance, take-off and landing, and maneuvering flight--the book focuses on the energy methods applied to path performance analysis. Throughout the text, numerous examples from both the commercial and military sectors show readers how the concepts and calculations are applied to real-life situations. Problems, ranging from basic to complex, test the readers' understanding and provide an opportunity for essential practice. To help focus the readers' attention on core issues, this text assumes that aerodynamics and propulsion are known inputs. Special appendices are provided to present some aerodynamic and propulsive equations and data. In general, topics are separated into horizontal and vertical plane approaches. Following an introduction and overview, basic energy concepts are employed to obtain a fundamental performance equation. This text, with its extensive use of examples and problem sets, is ideal for upper-level undergraduate and graduate students in engineering. It also serves as a reference for design engineers in both military and industrial sectors who want a set of clear and reliable methods to calculate aircraft performance. |
| 856 40 - ELECTRONIC LOCATION AND ACCESS | |
| Materials specified | Amazon.com |
| Uniform Resource Identifier | <a href="http://www.amazon.com/exec/obidos/ASIN/0470044160/chopaconline-20">http://www.amazon.com/exec/obidos/ASIN/0470044160/chopaconline-20</a> |
| Withdrawn status | Lost status | Source of classification or shelving scheme | Damaged status | Not for loan | Home library | Current library | Date acquired | Total Checkouts | Full call number | Barcode | Date last seen | Price effective from | Koha item type |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| Dewey Decimal Classification | Department of Mechanical and Aerospace Engineering Library | Department of Mechanical and Aerospace Engineering Library | 05/02/2012 | 621.132 SAA | 000130 | 05/02/2012 | 05/02/2012 | Book |