Jet Cooling of the Leading Edge of a Turbine Blade,
Abstract
One of the effective methods of the cooling of the leading edge of a turbine blade is jet blowing. In the reported experiments the object of the investigation was the model of a working blade made in a 5:1 scale with a chord of 60 mm. Parameters of the investigated system of jets were varied by means of an interchangeable nozzle part installed onto a permanent deflector.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jul 17, 1974
- Accession Number
- AD0784015
Entities
People
- A. I. Mazur
- V. E. Filipchuk
Organizations
- National Air and Space Intelligence Center