Genetic Algorithm-Based Optimisation of a Double-Wall Effusion Cooling System for a High-Pressure Turbine Nozzle Guide Vane (2024)

First Author: Van De Noort M
Attributed to:  Transpiration Cooling Systems for Jet Engine Turbines and Hypersonic Flight funded by EPSRC

Abstract

No abstract provided

Bibliographic Information

Digital Object Identifier: http://dx.doi.org/10.3390/ijtpp9010006

Publication URI: http://dx.doi.org/10.3390/ijtpp9010006

Type: Journal Article/Review

Parent Publication: International Journal of Turbomachinery, Propulsion and Power

Issue: 1