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2022 | OriginalPaper | Buchkapitel

Aeroelastic Models Design/Experiment and Correlation with New Theory

verfasst von : Deman Tang, Earl H. Dowell

Erschienen in: A Modern Course in Aeroelasticity

Verlag: Springer International Publishing

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Abstract

Several examples of experimental model designs, wind tunnel tests and correlation with new theory are presented in this chapter. The goal is not only to evaluate a new theory, new computational method or new aeroelastic phonomenon, but also to provide new insights into nonlinear aeroelastic phenomena, flutter, limit cycle oscillation (LCO), gust response and energy harvesting from a large flapping flag response. The experiments are conducted in a standard low speed wind tunnel. Similar experiments in a high speed wind tunnel would be very valuable.

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Vorheriges Kapitel Some Recent Advances in Nonlinear Aeroelasticity

Nächstes Kapitel Fluid/Structural/Thermal/Dynamics Interaction (FSTDI) in Hypersonic Flow

Recall that the buffet frequency is given in Fig. 9c as a function of flow velocity for the various angles of attack.

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Titel: Aeroelastic Models Design/Experiment and Correlation with New Theory
verfasst von: Deman Tang
Earl H. Dowell
Verlag: Springer International Publishing
Buch: A Modern Course in Aeroelasticity
Print ISBN: 978-3-030-74235-5

Electronic ISBN: 978-3-030-74236-2

Copyright-Jahr: 2022
DOI: https://doi.org/10.1007/978-3-030-74236-2_15

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