Zobrazeno 1 - 7
of 7
pro vyhledávání: '"Kenneth S. Dawson"'
Publikováno v:
Journal of Aircraft. 51:693-695
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::245f000543da67b38e0d127d1a8960d6
https://doi.org/10.2514/1.c032547
https://doi.org/10.2514/1.c032547
Autor:
Daniel L. Maxwell, Kenneth S. Dawson
Publikováno v:
Journal of Aircraft. 42:1588-1595
A conventional approach for flutter certification of asymmetric external store configurations on fighter aircraft is to analyze each side of the aircraft using half-span models. The flutter speed for the asymmetric configuration is then assumed to be
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b86cb87b727fac56ae11ab86dd4b2173
https://doi.org/10.2514/1.10693
https://doi.org/10.2514/1.10693
Publikováno v:
48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference.
Although Limit Cycle Oscillations have been investigated for many years, a practical method of predicting their amplitudes for a given configuration and flight condition has not yet been developed. Currently, linear analysis techniques are used to pr
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a2f1b4f6baa587851d4b8bd5e0544aa0
https://doi.org/10.2514/6.2007-2366
https://doi.org/10.2514/6.2007-2366
Limit Cycle Oscillation Prediction of Asymmetric External Store Configurations Using Neural Networks
Autor:
Daniel L. Maxwell, Kenneth S. Dawson
Publikováno v:
47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference 14th AIAA/ASME/AHS Adaptive Structures Conference 7th.
*A static artificial neural network is developed to predict limit cycle oscillation (LCO) amplitude levels and frequency of external store configurations on a fighter aircraft. This work is similar to previous networks generated by the authors with t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0f87b1d8353b03d3ae5caa69d03660f1
https://doi.org/10.2514/6.2006-1850
https://doi.org/10.2514/6.2006-1850
Autor:
Kenneth S. Dawson, Daniel L. Maxwell
Publikováno v:
2005 U.S. Air Force T&E Days.
A method for quantitatively comparing the Limit-Cycle Oscillatory motion for an F- 16 aircraft with varying external store carriage configurations is presented. The difficulty in understanding this motion for asymmetric configurations in particular i
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::59f3dad522f25c14c863e245a9244537
https://doi.org/10.2514/6.2005-7628
https://doi.org/10.2514/6.2005-7628
Autor:
Daniel L. Maxwell, Kenneth S. Dawson
Publikováno v:
45th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::451f5119d9cc1bccd7b8a22ef8cfe090
https://doi.org/10.2514/6.2004-1755
https://doi.org/10.2514/6.2004-1755
Autor:
Kenneth S. Dawson, Daniel L. Maxwell
Publikováno v:
44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference.
A conventional approach for flutter certification of asymmetric external store configurations on fighter aircraft is to analyze each side of the aircraft using half-span models. The flutter speed for the asymmetric configuration is then assumed to be
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b6f79d892a5d3727a264e70a5f570cc5
https://doi.org/10.2514/6.2003-1427
https://doi.org/10.2514/6.2003-1427