num_pages: 452
description: 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).
language: English
title: Aerothermodynamics of Gas Turbine Rocket Propulsion [With *]
publisher: AIAA (American Institute of Aeronautics & Ast