Leseprobe
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Aerodynamics of Turbines and Compressors. (HSA-1), Volume 1
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Naturwissenschaften, Medizin, Informatik, Technik / Technik
Beschreibung
Volume X of the High Speed Aerodynamics and Jet Propulsion series. Contents include: Theory of Two-Dimensional Flow through Cascades; Three-Dimensional Flow in Turbomachines; Experimental Techniques; Flow in Cascades; The Axial Compressor Stage; The Supersonic Compressor; Aerodynamic Design of Axial Flow Turbines; The Radial Turbine; The Centrifugal Compressor; Intermittent Flow Effects.
Originally published in 1964.
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Reciprocating engine, Turbocharger, Steam turbine, Supercharger, Lift coefficient, Perturbation theory (quantum mechanics), Overspeed (aeronautics), Vortex tube, Airfoil, Drag (physics), Dynamometer, Vortex ring, Stall (fluid mechanics), Helicopter rotor, Stator, Turbine blade, De Laval nozzle, Total pressure, Compressor stall, Engine tuning, Compressor characteristic, Centrifugal compressor, Turbomachinery, National Gas Turbine Establishment, Atmospheric pressure, Cylinder (geometry), Radial turbine, Turbojet, Kutta–Joukowski theorem, Laws of thermodynamics, Axial compressor, Flow coefficient, Hydraulic diameter, Nozzle, Continuity equation, Aircraft engine, Supersonic speed, Vortex sheet, Bearing (mechanical), Water injection (engine), Pressure gradient, Stagger (aeronautics), Wind tunnel, Equations of motion, Mach wave, Navier–Stokes equations, Turboprop, Aerodynamics, Boundary layer, Critical Mach number, Air–fuel ratio, Drag coefficient, Static pressure, Reynolds number, Throttle, Velocity triangle, Turbine, Volumetric flow rate, Gas compressor, Aspect ratio (aeronautics), Aerodynamic force, Mixed flow compressor, Mach reflection, Calculation, Engine test stand, Gas turbine, Jet propulsion, Differential equation, Mach number, Ideal gas law