Convected field analysis of flat panels response to turbulent boundary layer induced excitation-Reference-Cited by-同舟云学术

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Convected field analysis of flat panels response to turbulent boundary layer induced excitation

Published:2008-01 Issue:1 Volume:12 Page:91-104
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Vitiello P.,De Rosa S.,Franco F.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference35 articles.

1. A doublet lattice method for calculating lift distribution on oscillating surfaces in subsonic flow;Albano;AIAA Journal,1969

2. Anonymous, Aeroelasticity in MSC/NASTRAN – Seminar Notes, Mac-Neal Schwendler Corporation, 1993

3. Anonymous, MSC.NASTRAN User Guide

4. Application of the spectral finite element method to turbulent boundary layer induced vibration of plates;Birgersson;Journal of Sound and Vibration,2003

5. Aeroelasticity;Bisplinghoff,1995

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