Analysis of hydrodynamic unsteady turbulent flow structure in an aircraft power plant channels
- Authors: Kraev V.M.1, Myakochin A.S.1
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Affiliations:
- Moscow Aviation Institute (National Research University)
- Issue: Vol 60, No 2 (2017)
- Pages: 243-250
- Section: Aircraft and Rocket Engine Theory
- URL: https://journals.rcsi.science/1068-7998/article/view/230102
- DOI: https://doi.org/10.3103/S1068799817020131
- ID: 230102
Cite item
Abstract
The authors performed an experimental study of the effects of non-isothermal and unsteady hydrodynamic conditions on generation and evolution of turbulence. Measurements of the instantaneous axial and radial velocities and temperature in unsteady conditions, calculation of their average and pulsation magnitude, and their correlation were carried out. A physical model of the hydrodynamic unsteady turbulent flow was formulated based on the analysis of the frequency spectra of pulse parameters.
About the authors
V. M. Kraev
Moscow Aviation Institute (National Research University)
Email: info@pleiadesonline.com
Russian Federation, Volokolamskoe shosse 4, Moscow, 125993
A. S. Myakochin
Moscow Aviation Institute (National Research University)
Email: info@pleiadesonline.com
Russian Federation, Volokolamskoe shosse 4, Moscow, 125993