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Part I Analysis of a multi stage axial compressor with high reaction blading Part II A design study of a multi stage axial compressor with blading of high aspect ratio

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Figure

Figure L O shows the t o t 4 pressure v a r i a t i c ~ d o a g tkm blades after tke n o w has esoentidly settled inlo a ateads/ pattern
Figure 3. S t a t o r Axial irelocity Coefficients, = . 46000 .
Figure 4. Rotor Axial Velocity Coefficients, C$ : . 46000 .
Figure 5. Stator Axial Velocity Coefficients. 5 = . 69000 .
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