Aerothermodynamics of Gas Turbine and Rocket Propulsion
Author(s): Gordon Oates
This seminal book on gas turbine technology has been a bestseller since it was first published. It now includes a comprehensive set of software programs that complement the text with problems and design analyses. Software topics included are atmosphere programs, quasi-one-dimensional flow programs (ideal constant-area heat interaction, adiabatic constant-area flow with friction, rocket nozzle performance, normal shock waves, oblique shock waves), gas turbine programs (engine cycle analysis and engine off-design performance), and rocket combustion programs (Tc and PC given, He and PC given, isentropic expansion).
Product Information
General Fields
- :
- : American Institute of Aeronautics & Astronautics
- : 1.021
- : 31 December 1997
- : {"length"=>["23.5"], "width"=>["17.1"], "units"=>["Centimeters"]}
- : books
Special Fields
- : Gordon Oates
- : Hardback
- : English
- : 456