Year: 1989
Type: book
Abstract: A detailed examination of the cracking of aeroengine HP turbine blades has been carried out to determine the cause of cracking. Investigations point to design deficiency at the leading edge, particularly with regard to the orientation \nof the film cooling holes, as the most probable cause of failure.
Authors: Raghuram, AC, Krishnan, RV, Rangaraju, R, Venkataswamy, MA
Language: English
Subfield: Mechanical Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: green
OpenAlex ID: W58744724