Abstract Fundamental aerothermodynamic equations derived in Chapter 1 may now be applied for aerodynamic design of axial flow compressors and turbines. A typical sketch of an axial flow compressor is shown in Fig. 3-1.
Aerodynamic Design of Axial Flow Compressors and Turbines
Jet, Rocket, Nuclear, Ion and Electric Propulsion ; 2 ; 207-235
Applied Physics and Engineering ; 7 , 2
01.01.1968
29 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
Aerodynamic design and axial flow compressors
TIBKAT | 1965
|Aerodynamic design and axial flow compressors
SLUB | 1965
|Aerodynamic Design of Axial-Flow Compressors
NTRS | 1965
|Aerodynamic Loss Sources in Axial-Flow Compressors
NTIS | 1986
|