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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


A. R. Kirsanov
ОКБ им. А. Люльки
Russian Federation


References

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7. Kuzjmin M.V., Kirsanov A.R. Opisanie modeli razrushenija materiala rabochih lopatok ventiljatora. Nauchnihyj vestnik GosNII GA. 2012. № 4. Pp. 62-67. (In Russian).


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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ISSN 2079-0619 (Print)
ISSN 2542-0119 (Online)