INVESTIGATION OF AERO-ACOUSTIC EFFICIENCY OF THE FAN PROFILE OF THE TURBOJET ENGINE WITH THE USING ANSYS
The modification of aircraft engines is a complex process and such directions as investigation of the efficiency of the profile of the fan blade from the point of view of aero-acoustic characteristics require a special approach to the problem. One such approach is the use of a software environment t...
Main Authors: | М. И. Кисляк, М. М. Митрахович |
---|---|
Format: | Article |
Language: | English |
Published: |
National Aerospace University «Kharkiv Aviation Institute»
2017-07-01
|
Series: | Авіаційно-космічна техніка та технологія |
Subjects: | |
Online Access: | http://nti.khai.edu/ojs/index.php/aktt/article/view/1296 |
Similar Items
-
Results of experimental research of acoustic characteristics of acoustic liners for turbofan engines
by: Yevhen Rymarenko
Published: (2023-08-01) -
SELECTION AND JUSTIFICATION OF THE GRID GENERATION METHOD FOR FLOW SIMULATION IN A GAS TURBINE ENGINE FAN
by: Михаил Владимирович Хижняк, et al.
Published: (2020-08-01) -
Граничний стан осьового компресора ГТД, що експлуатується в умовах запиленої атмосфері
by: Двирник Я.В., et al.
Published: (2018-03-01) -
Discrete noise approximation of axial compressor and centrifugal fans
by: A P Alekseev
Published: (2009-06-01) -
The analysis of dependences for the estimation of centrifugal blad's machines noise
by: V K Mamaev, et al.
Published: (2009-06-01)