Symposium Papers, Volumes 1-2; Volume 9National Aeronautical Laboratory, 1989 - Aircraft gas-turbines |
Contents
Flanged Joints of Aeroengines | 624 |
Estimating to the Dynamic Behavior of RotorPedastalCasing Systems | 635 |
Response of the Simple Systems Damped by Real Dry Friction | 641 |
Copyright | |
48 other sections not shown
Other editions - View all
Common terms and phrases
aerodynamic afterbody AIAA aircraft amplitude analysis angle atomizer axial axisymmetric blade boundary layer calculation cascade characteristics coefficient combustion combustor components compressor computed configuration cowl damper decreases detonation wave diameter diffuser discrete tone distribution downstream droplet duct dynamic edge effects efficiency engine equations equivalence ratio exit experimental film flight Mach number flow field flow rate freestream frequency fuel injection gas turbine geometry grid heat high Mach hypersonic increase injection injector inlet intake interaction ISABE Ispf liquid Mach number mass flow mass flow rate maximum measured nozzle operating parameters performance plane predicted pressure ratio probe propfan propulsion system radial ramjet range region rotating rotor scramjet shock shown in Figure shows simulation speed spray squeeze film stagnation pressure static pressure supersonic surface swirl temperature thrust transonic turbofan turbojet turboramjet turborocket turbulent upstream v-gutter values variable viscosity vortex vorticity wall