Aerothermodynamics of Gas Turbine Rocket Propulsion [With *]

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).

Author: Gordon C. Oates, G. Oates, American Institute of Aeronautics and As
Publisher: AIAA (American Institute of Aeronautics & Ast
Published: 01/01/1997
Pages: 456
Binding Type: Hardcover
Weight: 1.88lbs
Size: 9.22h x 6.30w x 1.37d
ISBN13: 9781563472411
ISBN10: 1563472414
BISAC Categories:
- Technology & Engineering | Aeronautics & Astronautics
- Science | Mechanics | Thermodynamics
- Transportation | Aviation | General