Aerodynamics of Turbines and Compressors. (HSA-1), Volume 1
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Aerodynamic force
Aerodynamics
Age Group_Uncategorized
Age Group_Uncategorized
Aircraft engine
Airfoil
Air–fuel ratio
Aspect ratio (aeronautics)
Atmospheric pressure
automatic-update
Axial compressor
B01=William R. Hawthorne
Bearing (mechanical)
Boundary layer
Calculation
Category1=Non-Fiction
Category=TGBN
Category=TGMF1
Centrifugal compressor
Compressor characteristic
Compressor stall
Continuity equation
COP=United States
Critical Mach number
Cylinder (geometry)
De Laval nozzle
Delivery_Delivery within 10-20 working days
Differential equation
Drag (physics)
Drag coefficient
Dynamometer
Engine test stand
Engine tuning
eq_bestseller
eq_isMigrated=2
eq_nobargain
eq_non-fiction
eq_tech-engineering
Equations of motion
Flow coefficient
Gas compressor
Gas turbine
Helicopter rotor
Hydraulic diameter
Ideal gas law
Jet propulsion
Kutta–Joukowski theorem
Language_English
Laws of thermodynamics
Lift coefficient
Mach number
Mach reflection
Mach wave
Mixed flow compressor
National Gas Turbine Establishment
Navier–Stokes equations
Nozzle
Overspeed (aeronautics)
PA=Available
Perturbation theory (quantum mechanics)
Pressure gradient
Price_€100 and above
PS=Active
Radial turbine
Reciprocating engine
Reynolds number
softlaunch
Stagger (aeronautics)
Stall (fluid mechanics)
Static pressure
Stator
Steam turbine
Supercharger
Supersonic speed
Throttle
Total pressure
Turbine
Turbine blade
Turbocharger
Turbojet
Turbomachinery
Turboprop
Velocity triangle
Volumetric flow rate
Vortex ring
Vortex sheet
Vortex tube
Water injection (engine)
Wind tunnel
Product details
- ISBN 9780691624730
- Weight: 879g
- Dimensions: 152 x 235mm
- Publication Date: 21 Mar 2017
- Publisher: Princeton University Press
- Publication City/Country: US
- Product Form: Paperback
- Language: English
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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. The Princeton Legacy Library uses the latest print-on-demand technology to again make available previously out-of-print books from the distinguished backlist of Princeton University Press. These editions preserve the original texts of these important books while presenting them in durable paperback and hardcover editions. The goal of the Princeton Legacy Library is to vastly increase access to the rich scholarly heritage found in the thousands of books published by Princeton University Press since its founding in 1905.
