Principles of Aeroelasticity
(eBook)

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Published
Dover Publications, 2013.
ISBN
9780486151892
Status
Available Online

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eBook
Language
English

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APA Citation, 7th Edition (style guide)

Raymond L. Bisplinghoff., Raymond L. Bisplinghoff|AUTHOR., & Holt Ashley|AUTHOR. (2013). Principles of Aeroelasticity . Dover Publications.

Chicago / Turabian - Author Date Citation, 17th Edition (style guide)

Raymond L. Bisplinghoff, Raymond L. Bisplinghoff|AUTHOR and Holt Ashley|AUTHOR. 2013. Principles of Aeroelasticity. Dover Publications.

Chicago / Turabian - Humanities (Notes and Bibliography) Citation, 17th Edition (style guide)

Raymond L. Bisplinghoff, Raymond L. Bisplinghoff|AUTHOR and Holt Ashley|AUTHOR. Principles of Aeroelasticity Dover Publications, 2013.

MLA Citation, 9th Edition (style guide)

Raymond L. Bisplinghoff, Raymond L. Bisplinghoff|AUTHOR, and Holt Ashley|AUTHOR. Principles of Aeroelasticity Dover Publications, 2013.

Note! Citations contain only title, author, edition, publisher, and year published. Citations should be used as a guideline and should be double checked for accuracy. Citation formats are based on standards as of August 2021.

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Grouped Work ID2b70b9fd-bc9e-e2c0-9946-03ed82170f82-eng
Full titleprinciples of aeroelasticity
Authorbisplinghoff raymond l
Grouping Categorybook
Last Update2024-03-20 23:01:07PM
Last Indexed2024-03-27 23:59:07PM

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First LoadedJun 12, 2022
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Hoopla Extract Information

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    [synopsis] => Principles of Aeroelasticity constitutes an attempt to bring order to a group of problems which have coalesced into a distinct and mature subdivision of flight vehicle engineering. The authors have formulated a unifying philosophy of the field based on the equations of forced motion of the elastic flight vehicle. A distinction is made between static and dynamic phenomena, and beyond this the primary classification is by the number of independent space variables required to define the physical system.Following an introductory chapter on the field of aeroelasticity and its literature, the book continues in two major parts. Chapters 2 through 5 give general methods of constructing static and dynamic equations and deal specifically with the laws of mechanics for heated elastic solids, forms of aerodynamic operators, and structural operators. Chapters 6 through 10 survey the state of aeroelastic theory. The chapters proceed from simplified cases which have only a small, finite number of degrees of freedom, to one-dimensional systems (line structures), and finally to two-dimensional systems (plate- and shell-like structures).Chapter 9 combines some of the previous results by treating the unrestrained elastic vehicle in flight. All these chapters assume linear systems with properties independent of time, but Chapter 10 takes up the subject of systems which must be represented by nonlinear equations or by equations with time varying coefficients.
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