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Autor:
Jan R. Wright
Introduction to Aircraft Aeroelasticity and Loads, Second Edition is an updated new edition offering comprehensive coverage of the main principles of aircraft aeroelasticity and loads. For ease of reference, the book is divided into three parts and b
Autor:
Mehdi Sarmast, Jan R. Wright
Publikováno v:
Applied Mechanics and Materials. :1068-1073
Non-Linear Resonant Decay Method (NL-RDM) addresses the identification of multi-degree of freedom non-linear systems. This method offers a practical approach to the identification of lumped parameters and continuous systems by producing a non-linear
Publikováno v:
Journal of Aircraft. 46:1614-1626
The nonlinear resonant decay method identifies a nonlinear dynamic system using a model based in linear modal space comprising the underlying linear system and a small number of additional terms that represent the nonlinear behavior. In this work, th
Publikováno v:
Mechanical Systems and Signal Processing. 23:1037-1061
Over the past four decades considerable work has been done in the area of power spectrum estimation. The information contained within the power spectrum relates to a signal's autocorrelation or ‘second-order statistics’. The power spectrum provid
Publikováno v:
Mechanical Systems and Signal Processing. 23:8-29
The identification of non-linear dynamic systems is an increasingly important area of research, with potential application in many industries. Current non-linear identification methodologies are, in general, mostly suited to small systems with few de
Publikováno v:
Journal of Engineering Mechanics. 134:663-675
The behavior of humans jumping and bobbing on flexible structures has become a matter of some concern for both structural integrity and human tolerance. The issue is of great importance for a number of structure types including stadia terraces. A uni
Publikováno v:
Nuclear Engineering and Design. 237:1437-1444
A series of quench tests on hollow cylindrical specimens made of the machinable ceramic, Pyrophyllite, has been performed. The specimens consistently fractured with two diametrically opposite longitudinal cracks. Finite element analysis indicates tha
Autor:
Jan R. Wright, Jonathan E. Cooper
Publikováno v:
Introduction to Aircraft Aeroelasticity and Loads ISBN: 9781118700440
Introduction to Aircraft Aeroelasticity and Loads, Second Edition
Introduction to Aircraft Aeroelasticity and Loads, Second Edition
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::eefdc1c7530ea91a8e22b39ce24ca169
https://doi.org/10.1002/9781118700440.ch16
https://doi.org/10.1002/9781118700440.ch16
Autor:
Jan R. Wright, Jonathan E. Cooper
Publikováno v:
Introduction to Aircraft Aeroelasticity and Loads ISBN: 9781118700440
Introduction to Aircraft Aeroelasticity and Loads, Second Edition
Introduction to Aircraft Aeroelasticity and Loads, Second Edition
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c3c6e92d64f65fee4bf67eb7c0998052
https://doi.org/10.1002/9781118700440.ch21
https://doi.org/10.1002/9781118700440.ch21