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Basics of Fluid Mechanics, 2014a

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12.9. COMBINATION OF THE OBLIQUE SHOCK AND ISENTROPIC EXPANSION533<br />

δ, deflection angle<br />

60<br />

55<br />

50<br />

45<br />

40<br />

35<br />

30<br />

25<br />

20<br />

15<br />

10<br />

θδ - -Mach number relationship<br />

1.05<br />

1.10<br />

1.15<br />

1.20<br />

1.3<br />

1.4<br />

1.5<br />

1.6<br />

1.7<br />

1.8<br />

1.9<br />

2.0<br />

2.2<br />

2.4<br />

2.6<br />

2.8<br />

3.0<br />

3.2<br />

3.4<br />

3.6<br />

3.8<br />

4.0<br />

4.5<br />

5<br />

6<br />

7<br />

8<br />

9<br />

10<br />

15<br />

800<br />

k =1.4<br />

5<br />

0 10 20 30 40 50 60 70 80 90<br />

θ, shock angle<br />

December 4, 2007<br />

Fig. -12.20. The relationship between the shock wave angle, θ and deflection angle, δ, and<br />

Mach number for k=1.4. This figure was generate with GDC under command ./obliqueFigure<br />

1.4. Variety <strong>of</strong> these figures can be found in the biggest gas tables in the world provided<br />

separately in Potto Project.

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