Abstract
EVER increasing demand for high efficiencies from aircraft propulsion systems drives designers to continue to strive for the improved thermodynamic efficiencies attainable only by operating at ever higher absolute temperatures. In addition to significant developments in the materials used in the last two decades, engine components must be protected by forced cooling and boundary layer control strategies. Large numbers of accurately sized and positioned small holes are essential to direct cooling air to precise positions in accurately metered amounts.
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a callDisclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.
