Progress Towards Computational Method for Circulation Control Airfoils-Reference-Cited by-同舟云学术

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Progress Towards Computational Method for Circulation Control Airfoils

Published:2005-01-10 Issue: Volume: Page:
ISSN:
Container-title:43rd AIAA Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Swanson R.¹,Rumsey Christopher¹,Anders Scott¹

Affiliation:

1. NASA Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2005-89

Reference63 articles.

1. Anders,S.G,Sellers,W.L.,Washburn,A.E.\ActiveFlowControlActivitiesatNASALangley,"AIAA Paper 04-2623, 2004.

2. Jones,G.S.,andEnglar,R.J, \AdvancesinPneumatic-ControlledHigh-LiftSystemsThroughPulsedBlowing,"AIAA Paper 03-3411,2003.

3. Abramson, J. \Two-DimensionalSubsonicWind Tunnel Evaluationof Two RelatedCambered 15-PercentCirculation ControlAirfoils,"DTNSRDCASED-373,1977.

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1. Closed-loop computational fluid dynamics simulations with time-varying boundary conditions for circulation control;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2024-07-18

2. Fluidic Flow Control Devices for Gust Load Alleviation;Journal of Aircraft;2024-07

3. Dynamic Response of Circulation Control for Step and Sinusoidal Inputs;Journal of Aircraft;2023-11

4. Experimental load modification on a dual-slot circulation control airfoil;Experiments in Fluids;2022-12-21

5. Active Flow Control Devices for Wing Load Alleviation;Journal of Aircraft;2021-11-05

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