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Academic Journal
INVESTIGATION OF AERO-ACOUSTIC EFFICIENCY OF THE FAN PROFILE OF THE TURBOJET ENGINE WITH THE USING ANSYS
М. И. Кисляк, М. М. Митрахович
Авіаційно-космічна техніка та технологія, Vol 0, Iss 7, Pp 54-58 (2017)
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Title | INVESTIGATION OF AERO-ACOUSTIC EFFICIENCY OF THE FAN PROFILE OF THE TURBOJET ENGINE WITH THE USING ANSYS |
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Authors | М. И. Кисляк, М. М. Митрахович |
Publication Year |
2017
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Source |
Авіаційно-космічна техніка та технологія, Vol 0, Iss 7, Pp 54-58 (2017)
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Description |
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 that will allow to determine the most effective profile with minimal costs. This technique significantly speeds up the designer and research department, allowing for a minimum period of preliminary investigation of the parameters of the fan and take all the necessary measures.
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Document Type |
article
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Language |
English
Ukrainian |
Publisher Information |
National Aerospace University «Kharkiv Aviation Institute», 2017.
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Subject Terms | |