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
1968-01-01
29 pages
Article/Chapter (Book)
Electronic Resource
English
Aerodynamic design and axial flow compressors
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