FormulaDen.com
Physics
Chemistry
Math
Chemical Engineering
Civil
Electrical
Electronics
Electronics and Instrumentation
Materials Science
Mechanical
Production Engineering
Financial
Health
You are here
-
Home
»
Physics
»
Aerospace
»
Aerodynamics
Mach Number Behind Expansion Fan in Oblique Shock and Expansion Waves Formulas
Mach Number Behind Expansion Fan is the Mach number of downstream flow across the expansion fan. And is denoted by M
e2
.
Oblique Shock and Expansion Waves formulas that make use of Mach Number Behind Expansion Fan
f
x
Pressure Ratio across Expansion Fan
Go
f
x
Temperature Ratio across Expansion Fan
Go
f
x
Pressure behind Expansion Fan
Go
f
x
Temperature behind Expansion Fan
Go
f
x
Rearward Mach Angle of Expansion Fan
Go
f
x
Flow Deflection Angle due to Expansion Wave
Go
FAQ
What is the Mach Number Behind Expansion Fan?
Mach Number Behind Expansion Fan is the Mach number of downstream flow across the expansion fan.
Can the Mach Number Behind Expansion Fan be negative?
{YesorNo}, the Mach Number Behind Expansion Fan, measured in {OutputVariableMeasurementName} {CanorCannot} be negative.
Let Others Know
✖
Facebook
Twitter
Reddit
LinkedIn
Email
WhatsApp
Copied!