Symposium Papers, Volumes 1-2; Volume 13National Aeronautical Laboratory, 1997 - Aircraft gas-turbines |
Contents
Review and Comments on Ramjet Research in France | 3 |
Building on our Legacy of Excellence | 17 |
Changing the Landscape of Civil Aviation | 43 |
Copyright | |
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Common terms and phrases
aerodynamic AIAA aircraft airplane analysis angle axial blade row bleed boundary layer calculations CIAM coefficient combustion combustion efficiency combustor components compressor computational configuration cowl cycle diffuser downstream duct edge film effect equations equivalence ratio evaluation exit experimental Figure film cooling flight flow field flow rate fuel fuel injection gas turbine geometry grid heat transfer hole hydrogen hypersonic increase injection injector inlet intake integration ISABE leading edge Mach number mass flow mass flow rate measured mode nozzle ONERA operation parameters performance plane predicted pressure distribution pressure ratio pressure recovery propulsion system ramjet region rotating rotor scramjet shock shown in Fig shows simulation SNECMA speed static pressure stator subsonic supersonic surface temperature terminal shock test cell test facility thrust total pressure transonic turbine engine turbojet turbomachinery turbulence unsteady velocity Volvo Aero wake wall zone