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By:Jiri Cecrdle
Published on 2015-01-27 by Woodhead Publishing


Whirl flutter is the aeroelastic phenomenon caused by the coupling of aircraft propeller aerodynamic forces and the gyroscopic forces of the rotating masses (propeller, gas turbine engine rotor). It may occur on the turboprop, tilt-prop-rotor or rotorcraft aircraft structures. Whirl Flutter of Turboprop Aircraft Structures explores the whirl flutter phenomenon, including theoretical and practical as well as analytical and experimental aspects of the matter. The first introductory part gives a general overview regarding aeroelasticity, followed by the physical principle and the occurrence of whirl flutter in aerospace practice. The next section deals with experiment research including earlier activities performed, particularly from the sixties, as well as recent developments. Subsequent chapters discuss analytical methods such as basic and advanced linear models, and non-linear and CFD based methods. Remaining chapters summarize certification issues including regulation requirements, a description of possible certification approaches and several examples of aircraft certification from the aerospace practice. Finally, a database of relevant books and reports is provided. provides complex information of turboprop aircraft whirl flutter phenomenon presents both theoretical and practical (certification related) issues presents experimental research as well as analytical models (basic and advanced) of matter includes both early-performed works and recent developments contains a listing of relevant books and reports

This Book was ranked at 19 by Google Books for keyword mechanical engineering.

Book ID of Whirl Flutter of Turboprop Aircraft Structures's Books is D-QhBAAAQBAJ, Book which was written byJiri Cecrdlehave ETAG "bAD4XN63/2s"

Book which was published by Woodhead Publishing since 2015-01-27 have ISBNs, ISBN 13 Code is 9781782421863 and ISBN 10 Code is 1782421866

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Book which have "354 Pages" is Printed at BOOK under CategoryBusiness and Economics

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