Work

A numerical investigation of new film cooling hole configuration at the leading edge of asymmetrical turbine blade: part A

Year: 2012

Type: article

Source: Heat and Mass Transfer

DOI: 10.1007/s00231-012-1096-5

Author: Mustapha Benabed

Institution: Université des Sciences et de la Technologie d'Oran Mohamed Boudiaf

Language: English

Topic: Turbomachinery Performance and Optimization

Subfield: Aerospace Engineering

Field: Engineering

Domain: Physical Sciences

Open Access status: closed

OpenAlex ID: W2133340977

FWCI: 0.656

Cites: 14

Cited by: 1

Related to: 10