Numerical simulations of dynamic/aerodynamic interactions-Reference-Cited by-同舟云学术

Numerical simulations of dynamic/aerodynamic interactions

Published:1990-01 Issue:2-4 Volume:1 Page:461-482
ISSN:0956-0521
Container-title:Computing Systems in Engineering
language:en
Short-container-title:Computing Systems in Engineering

Author:

Mook D.T.,Nayfeh A.H.

Publisher

Elsevier BV

Subject

General Engineering

Reference64 articles.

1. An improved method for the prediction of completely three-dimensional aerodynamic load distributions on configurations with leading-edge vortex separation;Johnson;AIAA Paper No. 76-417,1976

2. Predictions of vortex-lift characteristics by a leading-edge suction analogy;Polhamus;Journal of Aircraft,1971

3. A vortex lattice method for general, unsteady aerodynamics;Konstadinopoulos;Journal of Aircraft,1985

4. Vortex-dominated conical-flow computations using unstructured adaptively-refined meshes;Batina;AIAA Paper No. 89-1816,1989

5. Implicit flux-split Euler schemes for unsteady aerodynamic analysis involving unstructured dynamic meshes;Batina;AIAA Paper No. 90-0936,1990

Cited by 7 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. A review on non-linear aeroelasticity of high aspect-ratio wings;Progress in Aerospace Sciences;2017-02

2. Dynamic Nonlinear Aeroelastic Analysis of the Joined Wing Configuration;53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference<BR>20th AIAA/ASME/AHS Adaptive Structures Conference<BR>14th AIAA;2012-04-23

3. Nonlinear-Aerodynamics/Nonlinear-Structure Interaction Methodology for a High-Altitude Long-Endurance Wing;Journal of Aircraft;2010-03

4. Nonlinear Krylov acceleration for CFD-based aeroelasticity;Journal of Fluids and Structures;2009-01

5. Time Domain Nonlinear Aeroelastic Analysis for HALE Wings;47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference<BR> 14th AIAA/ASME/AHS Adaptive Structures Conference<BR> 7th;2006-05