An extensive study of many aspects of the aerothermodynamics of aircraft gas turbine engines is presented. The study consists of twenty-six chapters writen by a total of twenty-four authors. After an initial comprehensive introductory chapter, the report provides a review of thermodynamics and gas dynamics and of laminar and turbulent flows. The cycle analysis of ideal engines is then considered, followed by the description of component losses and then the cycle analysis of non-ideal engines. Engine off-design performance is then considered followed by the description of engine/airplane matching. Succeeding chapters consider the behavior of the various components in detail. Major problem areas such as computation of turbomachinery boundary layers, aeroelasticity and unsteady aerodynamics, engine stability, engine noise, jet noise and finally the system aspects of engine installation are considered in detail. The document is intended to serve many purposes, including those of text, design manual, research reference and comprehensive overview of the aerothermodyns of aircraft gas turbine engines. (Peters)
The aerothermodynamics of aircraft gas turbine engines
Die Aerothermodynamik von Flugzeuggasturbinen
US Government Reports ; Jun ; 1-780
1978
780 Seiten
Report
Englisch
Aerothermodynamics of Aircraft Gas Turbine Engines
NTIS | 1978
|Aerothermodynamics of Pulsed Detonation Engines
British Library Conference Proceedings | 2000
|Aerothermodynamics of pulsed detonation engines
AIAA | 2000
|Aerothermodynamics of aircraft engine components
TIBKAT | 1985
|Springer Verlag | 2016
|