Tip vortex, stall vortex, and separation observations on pitching three-dimensional wings-Reference-Cited by-同舟云学术

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Tip vortex, stall vortex, and separation observations on pitching three-dimensional wings

Published:1993-07-06 Issue: Volume: Page:
ISSN:
Container-title:23rd Fluid Dynamics, Plasmadynamics, and Lasers Conference
language:
Short-container-title:

Author:

LORBER PETER¹

Affiliation:

1. United Technologies Research Center, East Hartford, CT

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1993-2972

Reference24 articles.

1. Dynamic stall on a three-dimensional rectangular wing

2. Comparisons in three-dimensionality in the unsteady flows elicited by straight and swept wings

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1. Blade Tip Vortex Characterization of a Rotor Under Cyclic Pitch Conditions Using BOS and PIV;AIAA Scitech 2019 Forum;2019-01-06

2. Tip-Vortex Dynamics of a Pitching Rotor Blade-Tip Model;AIAA Journal;2016-10

3. Dynamic Stall Simulations on a Pitching Finite Wing;34th AIAA Applied Aerodynamics Conference;2016-06-10

4. Comparison Between Two-Dimensional and Three-Dimensional Dynamic Stall;Notes on Numerical Fluid Mechanics and Multidisciplinary Design;2016

5. Investigation of three-dimensional dynamic stall on an airfoil using fast-response pressure-sensitive paint;Experiments in Fluids;2014-08-20

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