Design and Performance of Gas Turbine Power Plants
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Adiabatic flame temperature
Aerodynamic heating
Age Group_Uncategorized
Age Group_Uncategorized
Air compressor
Air preheater
Air-fuel ratio
automatic-update
Aviation fuel
Axial compressor
B01=Walter T. Olson
B01=William R. Hawthorne
Brake specific fuel consumption
Carbon dioxide
Catalysis
Catalytic combustion
Category1=Non-Fiction
Category=PH
Category=TGMF1
Category=TRP
Centrifugal compressor
Coke (fuel)
Combustion
Combustion analysis
Combustion chamber
Combustor
Compressor characteristic
Compressor stall
COP=United States
Cylinder (engine)
De Laval nozzle
Delivery_Delivery within 10-20 working days
Diesel fuel
Diffusion flame
Discharge coefficient
Ducted fan
Electrical resistivity and conductivity
Engine tuning
eq_bestseller
eq_isMigrated=2
eq_nobargain
eq_non-fiction
eq_science
Exhaust system
Flame holder
Fuel
Fuel gas
Fuel oil
Fuel tank
Gas analysis
Gas chromatography
Gas composition
Gas compressor
Gas duster
Gas generator
Gas meter
Gas turbine
Gas turbine locomotive
Heat of combustion
Heat transfer coefficient
Internal combustion engine cooling
Isothermal flow
Isothermal process
Language_English
Mach number
National Gas Turbine Establishment
Nozzle
PA=Available
Price_€100 and above
Propelling nozzle
PS=Active
Radiator (engine cooling)
Reciprocating engine
Reid vapor pressure
Safety factor (plasma physics)
softlaunch
Spark-ignition engine
Temperature-entropy diagram
Thermal expansion
Thermodynamic cycle
Thermodynamic equilibrium
Thermodynamic process
Thermodynamic temperature
Thermodynamics
Thrust specific fuel consumption
Traction (engineering)
Turbine
Turbine blade
Turbocharger
Vapor pressure
Yield (engineering)
Product details
- ISBN 9780691626154
- Weight: 794g
- Dimensions: 152 x 235mm
- Publication Date: 08 Dec 2015
- Publisher: Princeton University Press
- Publication City/Country: US
- Product Form: Paperback
- Language: English
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Volume XI of the High Speed Aerodynamics and Jet Propulsion series. Edited by W.R. Hawthorne and W.T. Olson. This is a comprehensive presentation of basic problems involved in the design of aircraft gas turbines, including sections covering requirements and processes, experimental techniques, fuel injection, flame stabilization, mixing processes, fuels, combustion chamber development, materials for gas turbine applications, turbine blade vibration, and performance. Originally published in 1960. 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.
