Zobrazeno 1 - 8
of 8
pro vyhledávání: '"Federico Roizner"'
Autor:
Federico Roizner, Moti Karpel
Publikováno v:
Journal of Aircraft. 56:1387-1397
The recently developed parametric flutter margin method is expanded to perform efficient sensitivity studies in which linear and nonlinear flutter characteristics are calculated for changes in sele...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::3b1f8945404883467df4a31fc33e5784
https://doi.org/10.2514/1.c035286
https://doi.org/10.2514/1.c035286
Publikováno v:
Journal of Aircraft. 56:228-238
The recently developed numerical parametric flutter margin method is applied to perform safe flutter tests in which the flutter-onset conditions of a nominal configuration are positively identified...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::c7f9f034d491271864845c4ee8f88576
https://doi.org/10.2514/1.c035045
https://doi.org/10.2514/1.c035045
Autor:
Federico Roizner, Moti Karpel
Publikováno v:
AIAA Journal. 56:1011-1022
A new parametric flutter margin method for linear and nonlinear stability analysis of aeroservoelastic systems is presented. The method is based on frequency-response calculations with the system s...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8362abf494a7e6542b1a4d4efda4904f
https://doi.org/10.2514/1.j056514
https://doi.org/10.2514/1.j056514
Publikováno v:
2018 AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f8105138cab8767a7dcfeb135d073953
https://doi.org/10.2514/6.2018-0704
https://doi.org/10.2514/6.2018-0704
Publikováno v:
58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ecfafa0b9bb24a963ae00c31246a345e
https://doi.org/10.2514/6.2017-0638
https://doi.org/10.2514/6.2017-0638
Autor:
Moti Karpel, Federico Roizner
Publikováno v:
58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::255a7cb9e6581f9eb2b384fbb6229c85
https://doi.org/10.2514/6.2017-1594
https://doi.org/10.2514/6.2017-1594
Publikováno v:
17th International Forum on Aeroelasticity and Structural Dynamics, IFASD 2017, 2017-June
Delft University of Technology
Delft University of Technology
The first experimental application of the Parametric Flutter Margin method for identification of aeroelastic instabilities is presented. The experiment was performed in two steps using a two degree-of-freedom wing model mounted in the wind tunnel. Fi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::0430944747268ef71b12fe5aa54d074b
http://resolver.tudelft.nl/uuid:6afb3f36-ec83-4f1f-8813-6fadf4d01ce3
http://resolver.tudelft.nl/uuid:6afb3f36-ec83-4f1f-8813-6fadf4d01ce3
Publikováno v:
Physics of Fluids. 28:054104
In this work, a transition scenario is demonstrated, in which most of the stages are followed analytically. The transition is initiated by the linear transient growth mechanism in plane Poiseuille flow subjected to an infinitesimally small secondary
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::323cd2d20d64a3d6ba2273382a541c37
https://doi.org/10.1063/1.4948307
https://doi.org/10.1063/1.4948307