Numerical approach to new tangential slot effect on film cooling effectiveness over asymmetrical turbine blade
Year: 2016
Type: article
Source: Thermophysics and Aeromechanics
Authors: Z. Senouci, M. Benabed
Language: English
Subfield: Aerospace Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
OpenAlex ID: W2567390287
