GENETIC ALGORITHM BASED OPTIMISATION OF A DOUBLE-WALL EFFUSION COOLING SYSTEM FOR A HIGH-PRESSURE TURBINE NOZZLE GUIDE VANE (2023)
Attributed to:
Transpiration Cooling Systems for Jet Engine Turbines and Hypersonic Flight
funded by
EPSRC
Abstract
No abstract provided
Bibliographic Information
Type: Other
Parent Publication: European Conference on Turbomachinery Fluid Dynamics and Thermodynamics, ETC
ISSN: 24104833 23130067