oblique

Obligue Shock Eguations

Glenn

Research

Center

Mach =M

Stagnation (Total) Conditions = t subscript

2

Zonę O

pressure =p temperaturę = T density =r Shock angle= s Wedge angle=a specific heat ratio = 1.4

cota = tans

6 M

5(M²sin²s -1)

- ¹jj M*sin^a(s-a) =

T _ (7M²sin²s - 1) (M²sin²s+ 5) ^To    36 M%in²s

^pti _ r 6 M²sin²s "Ir [•    6    -|f P,

P*o LM²sin²s+5 J 1.7 M^zsin²s - 1J p₀

M^in^ +5 7 M^zsin²s -1

6 M²si M²sin²s +5

M²sin²s -1

6