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(2017). Numerical Investigation of Aeroacoustic Phenomenon Flow over Tailless, Double, and Diamond Delta Wings, Using Large Eddy Simulation. Electronic and Cyber Defense, 5(1), 1-15.
. "Numerical Investigation of Aeroacoustic Phenomenon Flow over Tailless, Double, and Diamond Delta Wings, Using Large Eddy Simulation". Electronic and Cyber Defense, 5, 1, 2017, 1-15.
(2017). 'Numerical Investigation of Aeroacoustic Phenomenon Flow over Tailless, Double, and Diamond Delta Wings, Using Large Eddy Simulation', Electronic and Cyber Defense, 5(1), pp. 1-15.
Numerical Investigation of Aeroacoustic Phenomenon Flow over Tailless, Double, and Diamond Delta Wings, Using Large Eddy Simulation. Electronic and Cyber Defense, 2017; 5(1): 1-15.

Numerical Investigation of Aeroacoustic Phenomenon Flow over Tailless, Double, and Diamond Delta Wings, Using Large Eddy Simulation

مکانیک سیالات و آیرودینامیک
Article 2, Volume 5, Issue 1, January 1395, Pages 1-15    PDF (1.3 M)
Receive Date: 19 April 2017,  Revise Date: 22 February 2023,  Accept Date: 19 September 2018 
Keywords
Aeroacoustics; Diamond Delta Wing; Sound Pressure Level; Vortex Interactions; Large Eddy Simulation Approach; Strouhal Number
References
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  2. Verhaagen, N.G. “Effect of Leading Edge Radius on Aerodynamic Charecteristics of 50° Delta Wings”, AIAA Aerospace Sciences Meeting, Vol. 49, No. 2, pp. 858-871, 2011.
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  9. Taiebi-Rahni, M., Ramezanizadeh, M., Keimasi, M.R. “3-Dimensional Turbulent Incompressible Film Cooling Simulation, Using LES and RANS Approaches” Aerospace Mechanics Journal, Vol. 1, No. 3, pp. 11-20, 2006 (In Persian).
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  11. Ffowcs Williams, J.E. and Hawkings, D.L. “Sound Generation by Turbulence and Surface in Arbitrary Motion”, Philosophical Transaction of the Royal Society of London, Series A, Mathematical and Physical Sciences. Vol. 264, No. 1151, pp.321-342, 1969.
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  14. Tuccillo, R. and Notarnicola, L. “Aeroacoustic Methods for Low-Noise Technologies Design”, Faculty of Ingegneria Dipartimento di Meccanica Energetica, Nopoli, 2014.
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