Influence of Inlet Pressure Distortion on the Engine Performance of a Supersonic Passenger Aircraft

Author:

Alendar A. D.,Grunin A. N.,Evstigneev A. A.,Lanshin A. I.,Siluyanova M. V.

Publisher

Allerton Press

Subject

Industrial and Manufacturing Engineering,Mechanical Engineering

Reference14 articles.

1. Sum, Y. and Smith, H., Review and prospect of supersonic business jet design, Prog. Aerospace Sci., 2017, vol. 90, pp. 12–38.

2. Kazhan, V.G., Dunaevskii, A.I., Kosushkin, K.G., et al., The concept of a light supersonic administrative aircraft, in Problemy sozdaniya perspektiv aviatsionno-kosmicheskoi tekhniki (Problems of Creating Prospects for Aerospace Technology), Moscow: Fizmatlit, 2005, pp. 212–232.

3. Lyubimov, D.A., Kukshinova, I.V., and Vinogradov, V.A., RANS/ILES-method study of flow features in the spatial air intake of a supersonic business class aircraft in throttle modes, Teplofiz. Vys. Temp., 2021, no. 4, pp. 576–583.https://doi.org/10.31857/S0040364421040153

4. Vorob’eva, N.G. and Krasnov, S.E., On the mechanism of the influence of pressure heterogeneity on the stability of the GTE compressor, Tekh. Vozdush. Flota, 2011, vol. 85, no. 3 (704), pp. 41–46.

5. Krasnov, S.E., Minin, O.P., Olishevskii, D.A., and Shevel’kov, S.G., Computational study of the effect of an air intake of a complex spatial configuration on the operational characteristics of an aviation gas turbine engine with a high degree of double-circuit, Uch. Zap. Tsentr. Aerogidrodin. Inst., 2017, no. 3, pp. 34–41.

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