Navier-Stokes computations on swept-tapered wings, including flexibility-Reference-Cited by-同舟云学术

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Navier-Stokes computations on swept-tapered wings, including flexibility

Published:1990-04-02 Issue: Volume: Page:
ISSN:
Container-title:31st Structures, Structural Dynamics and Materials Conference
language:
Short-container-title:

Author:

GURUSWAMY GURU¹

Affiliation:

1. NASA, Ames Research Center, Moffett Field, CA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1990-1152

Reference28 articles.

1. Induced Wing Rock Oscillations of Slender Delta Wings," AIAA Paper 81-1883, August 1981. 2 Dobbs, S. K. and Miller, G. D. "Self-Induced Oscil

2. lation Wind Tunnel Test of a Variable Sweep Wing," AIAA Paper 85-0739, April 1985. 3 Mabey, D. G. "On the Prospects for Increasing Dy

3. Numerical Simulation of Transonic Separated Flow About the Complete F-16A," AIAA paper 88-2506,

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1. Fluid-Structure Interaction of HALE Wing Configuration with an Efficient Moving Grid Method;46th AIAA Aerospace Sciences Meeting and Exhibit;2008-01-07

2. Viscosity Influence on Flutter Boundary and Limit Cycle Oscillation in Transonic Regime;Journal of Fluid Science and Technology;2008

3. Calculation of Wing Flutter by a Coupled Fluid-Structure Method;Journal of Aircraft;2001-03

4. Aerodynamic Influence Coefficient Computations Using Euler/Navier-Stokes Equations on Parallel Computers;AIAA Journal;1999-11

5. Aeroelastic Computations on Wing-Body-Control Configurations on Parallel Computers;Journal of Aircraft;1998-03

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