Development of a high-fidelity transient aerothermal model for a helicopter turboshaft engine for inlet distortion and engine deterioration simulations

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Thesis Type: Postgraduate

Institution Of The Thesis: Orta Doğu Teknik Üniversitesi, Faculty of Engineering, Department of Aerospace Engineering, Turkey

Approval Date: 2012

Student: YAROSLAV NOVİKOV

Co-Supervisor: OĞUZ UZOL, ALİ TÜRKER KUTAY