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.

Keywords

• gas-turbine engine
• birdstrike capacity
• bird ingestion
• vulnerability
• destruction