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book (13)

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Dissertation
Theory and practice of flutter calucations for systems with many degrees of freedom.
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Year: 1952 Publisher: Leiden,

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Book
Means of compliance with Title 14 CFR, Part 23, [section] 23.629, Flutter
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Year: 2004 Publisher: [Washington, D.C.] : U.S. Dept. of Transportation, Federal Aviation Administration,

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Book
Damping formulas and experimental values of damping in flutter models
Authors: ---
Year: 1940 Publisher: Washington, [D.C.] : National Advisory Committee for Aeronautics,

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Book
A review of the two-dimensional problem of unsteady lifting surface theory during the last thirty years
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Year: 1953 Volume: 23 Publisher: s.l.] : [College Park,

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Book
Wind-tunnel study of deflected-elevator flutter encountered on a T-Tail airplane
Authors: --- --- ---
Year: 1969 Publisher: Washington, D.C. : National Aeronautics and Space Administration,

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Book
Dynamics of flexible aircraft : coupled flight mechanics, aeroelasticity, and control
Authors: ---
ISBN: 9781108354868 9781108420600 1108420605 Year: 2023 Publisher: Cambridge: Cambridge university press,

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"This text explores the interface between aeroelasticity, flight dynamics and control. Presenting concepts in a rigorous yet accessible way, the book builds up to state-of-the-art models through an intuitive step-by-step approach. It empowers the reader to design better, more eco-friendly aircraft, and features many hands on examples."


Book
Massbalancing of aircraft control surfaces
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Year: 1954 Publisher: London : Chapman & Hall Ltd.,

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Book
Large deflection panel flutter
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Year: 1962 Publisher: Delft : Technische Hogeschool Delft = Delft Technological University,

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Book
A method to stabilize linear systems using eigenvalue gradient information
Authors: --- ---
Year: 1985 Publisher: Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch,

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Book
Dynamics of flexible aircraft : coupled flight mechanics, aeroelasticity, and control
Authors: ---
ISBN: 1108359574 1108354866 Year: 2023 Publisher: Cambridge, United Kingdom ; New York, NY, USA : Cambridge University Press,

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Explore the connections among aeroelasticity, flight dynamics, and control with an up-to-date multidisciplinary approach. New insights into the interaction between these fields, which is a distinctive feature of many modern aircraft designed for very high aerodynamic efficiency, are fully illustrated in this one-of-a-kind book. Presenting basic concepts in a systematic and rigorous, yet accessible way, this book builds up to state-of-the-art models through an intuitive step-by-step approach. Both linear and nonlinear attributes are covered and, by revisiting classical solutions using modern analysis methods, this book provides a unique perspective to bridge the gap between disciplines. Numerous original numerical examples, including online source codes, help to build intuition through hands-on activities. This book will empower the reader to design better and more environmentally friendly aircraft, and is an ideal resource for graduate students, researchers, and aerospace engineers.

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