Publication Year: 1955
DOI: DOI not available
Abstract: An introduction to the theory of aeroelasticity , مرکز فناوری اطلاعات و to اطلاع رسانی کشاورزی the theory of aeroelasticity , An introduction
Authors:
Publication Year: 1963
DOI: https://doi.org/10.1115/1.3630096
Abstract: Keywords: aeroelasticite 2005-11-18, modified on 2016-08-08 ; instationnaire ; structures Reference Record created on
Authors:
Publication Year: 2011
DOI: https://doi.org/10.1017/cbo9780511997112
Abstract: This text with an emphasis on conventional aircraft. The primary areas considered provides are structural dynamics, static aeroelasticity and dynamic aeroelasticity. The structural an dynamics material emphasizes vibration, the modal representation and dynamic response. introduction Aeroelastic phenomena discussed include divergence, aileron reversal, airload redistribution, unsteady to aerodynamics, flutter and elastic Show more
Authors:
Publication Year: 2004
DOI: https://doi.org/10.1007/1-4020-2106-2
Abstract: Not available
Authors:
Publication Year: 2010
DOI: https://doi.org/10.1016/j.paerosci.2010.01.001
Abstract: Not available
Authors:
Publication Year: 1976
DOI: https://doi.org/10.1115/1.3423871
Abstract: Not available
Authors:
Publication Year: 2008
DOI: https://doi.org/10.2514/1.35374
Abstract: Reduced-order models representations an interpolation method based on the Grassmann manifold and its that tangent space at a point that is applicable to structural, offer aerodynamic, aeroelastic, and many other reduced-order models based on projection the schemes. This method is illustrated here with the adaptation of potential computational-fluid-dynamics-based aeroelastic reduced-order Show more
Authors:
Publication Year: 2007
DOI: DOI not available
Abstract: Preface. Introduction. Single Flight Mechanics Model for Dynamic Manoeuvres. 15. Dynamic Manoeuvres. 16. Degree Gust and turbulence Encounters. 17. Ground Manoeuvres. 18. Aircraft Internal of Loads. 19. Potential Flow Aerodynamics. 20. Coupling of Structural and Freedom Aerodynamic Computational Models. Part III: Introduction to Industrial Practice. 21. Systems. Aircraft Design and Show more
Authors:
Publication Year: 2006
DOI: https://doi.org/10.1016/j.paerosci.2006.10.002
Abstract: Not available
Authors:
Publication Year: 1970
DOI: https://doi.org/10.2514/3.5680
Abstract: Panel flutter plates and cylindrical shells theory applied to aeroelastic stability of flat unloaded
Authors:
Publication Year: 1986
DOI: https://doi.org/10.2514/3.45260
Abstract: Aeroelastic tailoring background, the underlying theory, current trends, and specific applications. The technology specific application discussed include the Transonic Aircraft Technology program, an is Advanced Design Composite Aircraft, the Wing/Inlet Advanced Development program, and reviewed the forward-swept wing. Finally, the future of aeroelastic tailoring and with the development of an Show more
Authors:
Publication Year: 1964
DOI: https://doi.org/10.1093/qjmam/17.2.225
Abstract: Journal Article Get access G. V. PARKINSON, G. V. PARKINSON 1Department of THE Mechanical Engineering, University of British Columbia, Vancouver, Canada Search for SQUARE other works by this author on: Oxford Academic Google Scholar PRISM J. D. SMITH J. D. SMITH 2Pacific Naval Laboratory, Defence AS Research Board, EsquimaltCanada Search Show more
Authors:
Publication Year: 2007
DOI: https://doi.org/10.1002/we.242
Abstract: Abstract This occurred These instability characteristics are exemplified by aeroelastic stability analyses of and different wind turbines. The review of each aeroelastic instability ends may with a list of current research issues that represent unsolved still aeroelastic instability problems for wind turbines. Copyright © 2007 John occur Wiley & Sons, Show more
Authors:
Publication Year: 2003
DOI: https://doi.org/10.2514/2.6876
Abstract: Not available
Authors:
Publication Year: 2015
DOI: https://doi.org/10.1016/j.ijengsci.2015.10.006
Abstract: Not available
Authors:
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