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Diffstat (limited to '3765/CH3/EX3.6/Ex3_6.sce')
-rw-r--r-- | 3765/CH3/EX3.6/Ex3_6.sce | 17 |
1 files changed, 17 insertions, 0 deletions
diff --git a/3765/CH3/EX3.6/Ex3_6.sce b/3765/CH3/EX3.6/Ex3_6.sce new file mode 100644 index 000000000..0ad8c2aa0 --- /dev/null +++ b/3765/CH3/EX3.6/Ex3_6.sce @@ -0,0 +1,17 @@ +clc +// Example 3.6.py +// Consider a point in a supersonic flow where the static pressure is 0.4 atm. When +// a pitot tube is inserted in the at this point, the pressure measured by the +// pitot tube is 3 atm. Calculate the mach number at this point. + +// Variable declaration +p1 = 0.4 // static pressure (in atm) +po2 = 3.0 // pressure measured by the pitot tube (in atm) + +//Calculations +// from table A2 for po2/p1 = 7.5 +M1 = 2.35 + +// Results +printf("\n Mach number is %.2f",(M1)) + |