Sample data from Engineering Database — 375 reference tables, deterministic calculators, and Engineering AI. Sign up free

Compressible Flow: NORMAL SHOCK

3 to 3.9

Compressible flow tables — isentropic, normal shock, Fanno (friction), Rayleigh (heat addition), and Prandtl-Meyer expansion flow relations as functions of Mach number for ideal gas with gamma=1.4. Mach range 0.01 to 50.

Mechanical Engineeringflow type: NORMAL SHOCK10 rowsPage 5 of 10
flow typemach numberM2 (dimensionless)T2 T1 (dimensionless)gamma (dimensionless)p02 p01 (dimensionless)p2 p1 (dimensionless)rho2 rho1 (dimensionless)
NORMAL SHOCK30.4751912.6790121.40.32834410.3333333.857143
NORMAL SHOCK3.10.4695342.7986031.40.30121111.0453.946612
NORMAL SHOCK3.20.4643492.9219921.40.27622911.784.031496
NORMAL SHOCK3.30.4595863.0491911.40.25327612.5383334.11202
NORMAL SHOCK3.40.45523.1802081.40.23222613.324.188406
NORMAL SHOCK3.50.4511543.3150511.40.21294814.1254.26087
NORMAL SHOCK3.60.4474133.4537281.40.19531214.9533334.329621
NORMAL SHOCK3.70.4439483.5962441.40.17919415.8054.394864
NORMAL SHOCK3.80.4407323.7426041.40.1644716.684.45679
NORMAL SHOCK3.90.4377423.8928131.40.15102717.5783334.515586

What else is in Engineering Database

Calculators that use this data

Related data