Calculations Related to Compressible AERODYNAMICScs

A) ISENTROPIC FLOW RELATIONS

insert
T0/T= P0/P= d0/d=
T/T*= P/P*= d/d*=
M number= M angle= A/A*=

 

B) NORMAL SHOCK RELATIONS

insert

                     M1=

T2/T1= M2=
P2/P1= D2/D1=

C) PITOT TUBE RELATIONS(MACHMETER)

insert p0/p=

D) OBLIQUE SHOCK RELATIONS

insert M1  

wave angle ßstrong= Mn2=
insert wave angle ßweak= M2=
Mn1= P2/P1= T2/T1=
deflection angle= d2/d1=  

E) EXPANSION WAVES (PRANDTL MEYER FUNCTION)

insert M1= v(M1)=