Comparison of Turbulence Models in Near Wake of Transport Plane C-130H Fuselage-Reference-Cited by-同舟云学术

Comparison of Turbulence Models in Near Wake of Transport Plane C-130H Fuselage

Published:2013-05 Issue:3 Volume:50 Page:847-852
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Pang Samuel K. H.¹,Ng E. Y. K.¹,Chiu W. S.¹

Affiliation:

1. Division of Thermal and Fluids Engineering, Nanyang Technological University, Singapore 639798, Republic of Singapore

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.C032031

Reference14 articles.

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2. SeegerM.MüllerL.CarlssonP. K.BuryY.PressignyY. L.LallemandG.VallanceM.WheelerR.BenneyR.CharlesR.MortonS. A.TavanS. “Four-Powers Long Term Technology Projects: ‘Airflow Influence on Airdrop’ and ‘2nd Precision Airdrop Improvements’,” AIAA Paper 2005-1602, 2005.

3. DES Turbulence Modelling on the C-130 Comparison Between Computational and Experimental Results

4. MortonS. A.VignesB.BuryY. “Experimental and Computational Results of a Simplified C-130 Shape Depicting Airflow Influence on Airdrop,” RTO MP-AVT-133 AC/323(AVT-133)TP/133, 2006.

5. Turbulence Modeling in Rotating and Curved Channels: Assessing the Spalart-Shur Correction

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