Near-Field Noise Prediction for Landing Gear Based on Detached Eddy Simulations

Ning Hu; Xuan Hao; Cheng Su; Wei Min Zhang; Han Dong Ma

doi:10.4028/www.scientific.net/AMM.472.105

Paper Titles

Resonance Reliability Analysis of Aeroengine Compressor Rotor Blade
p.79

Present Status of Damping Test Techniques for Magnesium Alloys
p.85

Parameter Sensitivity Analysis of Gear Contact in Gear-Bearing-Rotor System Based on Romax
p.91

Investigation of Crack Line Offset of Fracture Splitting Connecting Rod
p.100

Near-Field Noise Prediction for Landing Gear Based on Detached Eddy Simulations
p.105

Fatigue Life Analysis of Auger Stem in Soft Coal Seam
p.111

Research on Walking Principle of a Worm Pipe Robot
p.115

Harvester Threshing Device Parameters Modular Design Based on Solidworks
p.120

A New Way to Simulate the Fluid Structure Interaction between the Bioprosthetic Heart Valve and Blood: FE-SPH Method
p.125

HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vol. 472Near-Field Noise Prediction for Landing Gear Based...

Near-Field Noise Prediction for Landing Gear Based on Detached Eddy Simulations

Abstract:

A four-wheel rudimentary landing gear is studied numerically by detached eddy simulation (DES) based on the Spalart-Allmaras turbulence model. The surface sound pressure level and sound pressure spectra are calculated using the obtained unsteady flow field. The investigation shows that DES can describe the steady and unsteady properties in the flow around rudimentary landing gear. It can give reasonable results since the flow around the landing gear is a massive separated flow. The results prove the feasibility of DES type methods in massive separated unsteady flow field and aerodynamic noise prediction for landing gear, and can be used in the study of landing gear noise reduction.

You might also be interested in these eBooks

View Preview

Info:

Periodical:

Applied Mechanics and Materials (Volume 472)

Pages:

105-110

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.472.105

Citation:

Cite this paper

Online since:

January 2014

Authors:

Ning Hu, Xuan Hao, Cheng Su, Wei Min Zhang, Han Dong Ma

Keywords:

Detached Eddy Simulation, Landing Gear, Noise, Unsteady Flow

Export:

RIS, BibTeX

Price:

Permissions CCC:

Request Permissions

Permissions PLS:

Request Permissions

Сopyright:

Citation:

References

[1] S.L. Long, H. Nie, C.J. Xue and X. Xu. Acta Aeronautica et Astronautica Sinica. 2012; 33(6): 1002-1013.

Google Scholar

[2] W.M. Zhang, X. Hao, D.B. Chen and J.J. Zhou. Aeronautical Manufacturing Technology. 2010; 14: 58—61.

Google Scholar

[3] S.L. Long, H. Nie and X. Xu. Applied Mechanics and Materials, 2012; 18: 184-185.

Google Scholar

[4] Z.X. Xiao, J. Liu, K.Y. Luo. J.B. Huang and S. Fu. AIAA Journal, 2013; 51(1): 107-125.

Google Scholar

[5] Proceedings (CDROM) of the AIAA-NASA Workshop on Benchmark Problems for Airframe Noise Computations-I (BANC-1)[C] Stockholm, Sweden, June 0-11, (2010).

Google Scholar

[6] L. Ventkatakrishnam, N. Karthikeyan and K. Meija. AIAA 2011-354.

Google Scholar

[7] P.R. Spalart. Annual Review of Fluid Dynamics, 2009; 41: 181 – 202.

Google Scholar

[8] P.R. Spalart, W. -H. Jou, M. Strelets and S.R. Allmaras. Advances in DNS/LES, (1997).

Google Scholar

[9] P.R. Spalart. NASA contractor report NASA/CR-2001-211032, (2001).

Google Scholar

[10] S. Krajnović, R. Lárusson, E. Helgason and B. Basara. 6th AIAA Theoretical Fluid Mechanics Conference, 27 - 30 June 2011, Honolulu, Hawaii.

Google Scholar