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Publicado por Takveen, Inc. July 2006, 2006
ISBN 10: 0977073939ISBN 13: 9780977073931
Librería: Dunaway Books, St. Louis, MO, Estados Unidos de America
Libro
Paper Back. Condición: Good. paperback.
Publicado por Takveen, Inc., 2006
ISBN 10: 0977073920ISBN 13: 9780977073924
Librería: Ergodebooks, Houston, TX, Estados Unidos de America
Libro
Paperback. Condición: Good.
Publicado por Takveen, Inc., 2006
ISBN 10: 0977073939ISBN 13: 9780977073931
Librería: Ergodebooks, Houston, TX, Estados Unidos de America
Libro
Paperback. Condición: Used: Good.
Publicado por Takveen, Inc., 2007
ISBN 10: 0977073963ISBN 13: 9780977073962
Librería: Bookmans, Tucson, AZ, Estados Unidos de America
Libro
Paperback. Condición: Good. Satisfaction 100% guaranteed.
Publicado por Takveen, 2008
ISBN 10: 097707398XISBN 13: 9780977073986
Librería: Bookmonger.Ltd, HILLSIDE, NJ, Estados Unidos de America
Libro
paperback. Condición: Very Good. Crease on cover*.
Publicado por LAP Lambert Academic Publishing, 2011
ISBN 10: 384433078XISBN 13: 9783844330786
Librería: Ria Christie Collections, Uxbridge, Reino Unido
Libro Impresión bajo demanda
Condición: New. PRINT ON DEMAND Book; New; Fast Shipping from the UK. No. book.
Publicado por LAP Lambert Academic Publishing 2011-04, 2011
ISBN 10: 384433078XISBN 13: 9783844330786
Librería: Chiron Media, Wallingford, Reino Unido
Libro
PF. Condición: New.
Publicado por LAP LAMBERT Academic Publishing, 2011
ISBN 10: 384433078XISBN 13: 9783844330786
Librería: Lucky's Textbooks, Dallas, TX, Estados Unidos de America
Libro
Condición: New.
Publicado por LAP LAMBERT Academic Publishing Apr 2011, 2011
ISBN 10: 384433078XISBN 13: 9783844330786
Librería: BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, Alemania
Libro Impresión bajo demanda
Taschenbuch. Condición: Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -Flight flutter testing is mandatory for aircraft certification; however it is a risky, lengthy and costly process with ever-growing demand for shorter and cheaper as well as online testing tools. This research has dealt with two key issues and the methods developed have been validated on simulated aeroelastic data sets. Firstly, the flutter boundaries are evaluated using statistical confidence criteria based on Least Squares statistics and eigenvalue perturbation theory rooting from noise statistics in the response data from a single flight test outdoing the need for Monte Carlo simulations or repeated tests. The approach is employed on three different flutter prediction tools: Damping Extrapolation method, Flutter Margin method and Envelope Function method. Results from the first two methods showed widening of the confidence bounds with increasing noise whilst the third method remained robust to it. The other research problem involves the development of an online flutter prediction tool using the Envelope Function method. The original approach is extended by making direct use of the chirp response to predict the flutter speed and is applicable to both offline and online versions. 248 pp. Englisch.
Publicado por LAP LAMBERT Academic Publishing, 2011
ISBN 10: 384433078XISBN 13: 9783844330786
Librería: AHA-BUCH GmbH, Einbeck, Alemania
Libro Impresión bajo demanda
Taschenbuch. Condición: Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - Flight flutter testing is mandatory for aircraft certification; however it is a risky, lengthy and costly process with ever-growing demand for shorter and cheaper as well as online testing tools. This research has dealt with two key issues and the methods developed have been validated on simulated aeroelastic data sets. Firstly, the flutter boundaries are evaluated using statistical confidence criteria based on Least Squares statistics and eigenvalue perturbation theory rooting from noise statistics in the response data from a single flight test outdoing the need for Monte Carlo simulations or repeated tests. The approach is employed on three different flutter prediction tools: Damping Extrapolation method, Flutter Margin method and Envelope Function method. Results from the first two methods showed widening of the confidence bounds with increasing noise whilst the third method remained robust to it. The other research problem involves the development of an online flutter prediction tool using the Envelope Function method. The original approach is extended by making direct use of the chirp response to predict the flutter speed and is applicable to both offline and online versions.
Publicado por LAP LAMBERT Academic Publishing, 2011
ISBN 10: 384433078XISBN 13: 9783844330786
Librería: moluna, Greven, Alemania
Libro Impresión bajo demanda
Condición: New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. Autor/Autorin: Abbasi AsimDr Abbasi did Bachelors in Mechanical Engineering from University of Engineering and Technology, Taxila, Pakistan in 1999 and PhD in Aeronautical Engineering from University of Manchester, UK in 2009. His main research int.
Publicado por LAP LAMBERT Academic Publishing, 2011
ISBN 10: 384433078XISBN 13: 9783844330786
Librería: PBShop.store US, Wood Dale, IL, Estados Unidos de America
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PAP. Condición: New. New Book. Shipped from UK. THIS BOOK IS PRINTED ON DEMAND. Established seller since 2000.
Publicado por LAP LAMBERT Academic Publishing, 2011
ISBN 10: 384433078XISBN 13: 9783844330786
Librería: PBShop.store UK, Fairford, GLOS, Reino Unido
Libro Impresión bajo demanda
PAP. Condición: New. New Book. Delivered from our UK warehouse in 4 to 14 business days. THIS BOOK IS PRINTED ON DEMAND. Established seller since 2000.
Publicado por LAP LAMBERT Academic Publishing, 2011
ISBN 10: 384433078XISBN 13: 9783844330786
Librería: Mispah books, Redhill, SURRE, Reino Unido
Libro
Paperback. Condición: Like New. Like New. book.