Fluid Mechanics        

                                         

Fluid Mechanics lets you easily calculate compressible gas flow parameters for isentropic and normal shockwave flow.

 

Features:


1. Isentropic flow Input parameters – gas constant ɤ (Cp/Cv,) and one of the following ** ten ** parameters:


• Mach number 

• A/A*  (subsonic or supersonic)

• T/To

• P/Po

• ρ/ρo

• P/P*

• T/T*

• ρ/ρ*

• Mach angle

• Prandtl-Meyer angle


2. Isentropic flow Output parameters:


• Mach number

• A/A*

• T/To

• P/Po

• ρ/ρo

• P/P*

• T/T*

• ρ/ρ*

• Mach angle

• Prandtl-Meyer angle


3. Normal Shockwave flow Input parameters – gas constant ɤ (Cp/Cv), and one of the following ** seven ** parameters:


• Mach number upstream of shock (M1)
• Mach number downstream of shock (M2)

• P2/P1

• T2/T1

• ρ2/ρ1

• Po2/Po1

• P1/Po2


4. Normal Shockwave flow Output parameters:


• Mach number upstream of shock (M1)
• Mach number downstream of shock (M2)

• P2/P1

• T2/T1

• ρ2/ρ1

• Po2/Po1

• P1/Po2


5. Easily toggle between static-to-stagnation and stagnation-to-static ratios.


6. A user's guide is provided within the in-program help.


7. Intuitive user interface.

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