METHOD OF ACOUSTIC PRESSURE ESTIMATION GENERATED BY THE AVIATION GAS-TURBINE ENGINE FAN

Authors

  • Ю. Терещенко National Aviation University
  • К. Дорошенко National Aviation University

DOI:

https://doi.org/10.18372/2310-5461.6.5170

Keywords:

method, acoustic pressure, fan

Abstract

Method of acoustic pressure estimation generated by the aviation gas-turbine engine fan, taking into account values of fan’s efficiency, were developed. A method is based on the numeral experiment.

 

References

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Токарев В. И. и др. Снижение шума при эксплуатации пассажирских самолетов / В. И. Токарев и др. — К. : Техника, 1990. — 127 с.

Yamagata A. CFD Prediction of Unsteady Pressures due to Fan Rotor-Stator Interac tion, ISABE. 2003. — № 2003 / A. Yamagata, H. Kodama, N. Tsuchiya. — 130 р.

Голдстейн Е. Аэроакустика / Е. Голдстейн. — М. : Машиностроение, 1981. — 295 с.

Терещенко Ю. М. Авіаційні газотурбінні двигуни / Ю. М. Терещенко, М. М. Мітрахович; за ред. Ф. М. Муравченко. — К. : КВІЦ, 2001. — 311 с.

Акустическая динамика машин и конструкций: сб. статей. — М. : Наука, 1973. — 112 с.

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Published

2010-12-14

How to Cite

Терещенко, Ю., & Дорошенко, К. (2010). METHOD OF ACOUSTIC PRESSURE ESTIMATION GENERATED BY THE AVIATION GAS-TURBINE ENGINE FAN. Science-Based Technologies, 6(2), 5–9. https://doi.org/10.18372/2310-5461.6.5170

Issue

Vol. 6 No. 2 (2010)

Section

Avionics and Engineering

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