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Main \ Results \ Compressible flows \ Transsonic flow in a plane compressor cascade

• Plane compressor cascade. Angle of attack 0. Mach and pressure distibution
• Flow development in a plane compressor cascade. Angles of attack 0 and 5. Mach distibution

  Mach contours	Pressure distribution

  
  

  Mach contours
  Angle of attack 0	Angle of attack 5

  
  
  

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