Approximation of unsteady aerodynamic forces Q(k,M) by use of fuzzy techniques-Reference-Cited by-同舟云学术

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Approximation of unsteady aerodynamic forces Q(k,M) by use of fuzzy techniques

Published:2005-04-18 Issue: Volume: Page:
ISSN:
Container-title:46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
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Author:

Hiliuta Adrian¹,Botez Ruxandra¹,Brenner Martin²

Affiliation:

1. Ecole de Technologie Superieure

2. NASA Dryden

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2005-2079

Reference7 articles.

1. 2Rodden,WP,Harder,RL,andBellinger,ED."AeroelasticAdditiontoNASTRAN,"NASACR-3094,1979.

2. 3Tiffany, SH and Adams, WM. "Nonlinear programming extensions to rational function approximation of unsteady aerodynamics," NASA TP-2776,July1988.

Cited by 2 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Improved Method for Creating Time-Domain Unsteady Aerodynamic Models;Journal of Aerospace Engineering;2007-07

2. Aerodynamic forces based on an error analytical formulation for aeroservoelasticity studies on an F/A-18 aircraft;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2006-05-01

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