ARAMA SONUÇLARI

Toplam 4 adet sonuçtan 4 tanesi görüntülenmektedir.

Aerothermal Optimization of Film Cooling Hole Locations on the Squealer Tip of an HP Turbine Blade

Journal of Thermal Science and Engineering Applications, Vol. 16, No. 5, Mart 2024, s. 1-20, ISSN: 1948-5085

YILDIZ FARUK,ALPMAN EMRE,KAVURMACIOĞLU LEVENT ALİ,CAMCI CENGİZ

An aerothermal study of the influence of squealer width and height near a HP turbine blade

International Journal of Heat and Mass Transfer, Vol. 120, Mayıs 2018, s. 18-32, ISSN: 0017-9310

ŞENEL CEM BERK,MARAL HIDIR,KAVURMACIOĞLU LEVENT ALİ,CAMCI CENGİZ

Casing grooves to improve aerodynamic performance of a HP turbine blade

Aerospace Science and Technology, Vol. 76, Mayıs 2018, s. 194-203, ISSN: 1270-9638

KAVURMACIOĞLU LEVENT ALİ,ŞENEL CEM BERK,MARAL HIDIR,CAMCI CENGİZ

Performance of Partial and Cavity Type Squealer Tip of a HP Turbine Blade in a Linear Cascade

International Journal of Aerospace Engineering, Vol. 2018, Ocak 2018, s. 1-11, ISSN: 1687-5966

KAVURMACIOĞLU LEVENT ALİ,MARAL HIDIR,ŞENEL CEM BERK,CAMCI CENGİZ