Investigation of Lighthill-Source Components in a Planar Jet-Wing-Flap Configuration
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Publisher
Springer International Publishing
Link
https://link.springer.com/content/pdf/10.1007/978-3-030-79561-0_72
Reference13 articles.
1. Belyaev, I.V., Zaytsev, M.Y., Kopiev, V.F., Ostrikov, N.N., Faranosov, G.A.: Studying the effect of flap angle on the noise of interaction of a high-bypass jet with a swept wing in a co-flow. Acoust. Phys. 63(1), 14–25 (2017). https://doi.org/10.1134/S1063771016060026
2. Colonius, T., Freund, J.B.: Application of lighthill’s equation to a mach 1.92 turbulent jet. AIAA J. 38, 368–370 (2000)
3. Crighton, D.G.: Basic principles of aerodynamic noise generation. Prog. Aerosp. Sci. 16, 31–96 (1975)
4. Faranosov, G., Kopiev, V., Ostrikov, N., and Kopiev, V.: The effect of pylon on the excess jet-flap interaction noise. In: Proceedings of the 22nd AIAA/CEAS Aeroacoustics Conference, AIAA Paper 2016-3043, Lyon, France (2016)
5. Freund, J.B.: Noise sources in a low-reynolds-number turbulent jet at mach 0.9. J. Fluid Mech. 438, 277–305 (2001)
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