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Experimental investigation of a Y-shaped engine inlet at subsonic flow conditions

Part of: ISABE 2024

Published online by Cambridge University Press:  24 April 2024

U.C. Küçük Open the ORCID record for U.C. Küçük [Opens in a new window]
U.C. Küçük*
Affiliation:
Propulsion Aerodynamics, Turkish Aerospace, Ankara, Turkey
*
Email: kucukumutcan@gmail.com
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Abstract

In this paper, the results of an experimental investigation for a Y-shaped engine inlet are presented. The experiment is performed at subsonic flow conditions. The main focus is given to time-dependent total pressures measured at the aerodynamic interface plane. Distinctive frequencies carrying high energy contents of the fluctuating total pressures are given and the relation between time-dependent and time-average performance parameters is presented. The cross-correlation coefficients of the high frequency probe readings distributed through the aerodynamic interface plane are also investigated.

Keywords

Aeroenginewind tunnel testsspectral analysisengine integrationcompatibilityinlet aerodynamics
Type
Research Article
Information
The Aeronautical Journal , Volume 128 , Special Issue 1325: The Aeronautical Journal ISABE 2024 Special Issue , July 2024 , pp. 1417 - 1428
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Copyright
© The Author(s), 2024. Published by Cambridge University Press on behalf of Royal Aeronautical Society

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