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name “aeroelasticity” to describe these phenomena, which are the subject of this text. In the design of aerospace vehicles, aeroelastic phenomena can result ...
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www.loc.gov/catdir/samples/cam031/2001052552.pdf
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This report describes the development of an aeroelastic model capable of representing in an approximate manner the fundamental nonlinear aeroelastic ...
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www.stormingmedia.us/17/1728/A172894.html
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These experiments are unique in terms of the model scaling and characteristics, the range of Mach number and dynamic pressure and the observed phenomena. To date, the analysis of the data performed with the support of AFOSR yielded two journal articles and two conference papers.
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www.stormingmedia.us/69/6958/A695824.html
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A global model is identified inclusive of any whatsoever aeroelastic phenomenon, the linearization of which allows study of incipient aerodynamic ...
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linkinghub.elsevier.com/retrieve/pii/016761059390139F
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As the most important aeroelastic phenomena, e.g. flutter and divergence, ... [5] classically define the range of aeroelastic phenomena through their ...
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linkinghub.elsevier.com/retrieve/pii/S0376042107000462
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Aeroelasticity is the science which studies the interaction among inertial elastic and aerodynamic forces It was defined by Collar in 1947 as the study of the mutual interaction that takes place within the triangle of the inertial elastic and aerodynamic forces acting on structural members exposed to an airstream and the ...
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en.allexperts.com/e/a/ae/aeroelasticity.htm
en.allexperts.com/e/a/ae/aeroelasticity.htm
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The parameters of training jets are usually at the lower limit of the transonic region. ... Title : Some Problems of Modelling Aeroelastic Phenomena in a Transonic Tunnel,
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stinet.dtic.mil/oai/oai?&verb=getRecord&metadataPrefix=...
stinet.dtic.mil/oai/oai?&verb=getRecord&metadataPrefix=html&identifier=ADA007391
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Accession Number : ADA053931 ... Descriptive Note : Technical rept., ... Corporate Author : GENERAL MOTORS CORP INDIANAPOLIS IND DETROIT DIESEL ALLISON DIV...
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stinet.dtic.mil/oai/oai?verb=getRecord&metadataPrefix=h...
stinet.dtic.mil/oai/oai?verb=getRecord&metadataPrefix=html&identifier=ADA053931
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Structural nonlinearities such as freeplay and large deformation effects are considered in the present aeroelastic analysis system. Finally, aeroelastic characteristics of several flight vehicles will be explained considering both aerodynamic and structural nonlinearities.
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adsabs.harvard.edu/abs/2009MPLB...23..421L
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