VALIDATION OF AIRCRAFT GAS-TURBINE ENGINE INLET BIRD THROW-IN SIMULATION MODEL
Abstract
This article describes validation procedure of the birds throw into gas-turbine engine (GTE) simulation model and the preceding verification of its main components. The provided data are including predictive and experimental data, as an additional documentary proof of the simulation model fidelity, repeatability and sensitivity.
About the Authors
M. V. Kuzmin
ОКБ им. А. Люльки
Russian Federation
Russian Federation
A. R. Kirsanov
ОКБ им. А. Люльки
Russian Federation
Russian Federation
References
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Review
For citations:
Kuzmin M.V., Kirsanov A.R. VALIDATION OF AIRCRAFT GAS-TURBINE ENGINE INLET BIRD THROW-IN SIMULATION MODEL. Civil Aviation High Technologies. 2015;(212):120-126. (In Russ.)
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