Investigation of Near-Field Flow Unsteadiness Around a NACA0012 Wingtip Using Large-Eddy-Simulation Approach-Reference-Cited by-同舟云学术

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Investigation of Near-Field Flow Unsteadiness Around a NACA0012 Wingtip Using Large-Eddy-Simulation Approach

Published:2010-01-04 Issue: Volume: Page:
ISSN:
Container-title:48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition
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Author:

Imamura Taro¹,Hirai Tohru²,Enomoto Shunji¹,Yokokawa Yuzuru¹,Kato Hiroyuki¹,Yamamoto Kazuomi¹

Affiliation:

1. Japan Aerospace Exploration Agency (JAXA)

2. Ryoyu Systems Company, Ltd.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2010-10

Reference25 articles.

1. Hardin,J.C."Airframe self-noise:Fouryears ofresearch;aircraft noisereductionforcommercial aircraft,"NASA-TM-X73908,Jul 1976.

2. Streett,C.L.,Lockard,D.P.,Singer,B.A.,Khorrami,M.R.,andChoudhari,M.M."InSearchofthePhysics:TheInterplay of Experiment and ComputationinAirframe NoiseResearch;Flap-Edge Noise"AIAA Paper 2003-977,Jan. 2003.

3. Choudhari,M.,andKhorrami,M.R."ComputationalStudyof PorousTreatmentforAlteringFlapSide-EdgeFlowField", AIAA Paper 2003-3113,May2003.

4. Streett,C.L."NumericalSimulationofFluctuationsLeadingtoNoiseinaFlap-EdgeFlowfield",AIAAPaper98-0628,Jan. 1998.

5. Street,C.L."NumericalSimulationAFlap-edgeFlowfield",AIAApaper98-2226,June1998.

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