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
Prandtl Meyer Function at Downstream Mach no. in Oblique Shock and Expansion Waves Formulas
Prandtl Meyer Function at Downstream Mach no. is the Prandtl Meyer Functional value at downstream of expansion wave. And is denoted by v
M2
. Prandtl Meyer Function at Downstream Mach no. is usually measured using the Degree for Angle. Note that the value of Prandtl Meyer Function at Downstream Mach no. is always negative.
Oblique Shock and Expansion Waves formulas that make use of Prandtl Meyer Function at Downstream Mach no.
f
x
Flow Deflection Angle using Prandtl Meyer Function
Go
FAQ
What is the Prandtl Meyer Function at Downstream Mach no.?
Prandtl Meyer Function at Downstream Mach no. is the Prandtl Meyer Functional value at downstream of expansion wave. Prandtl Meyer Function at Downstream Mach no. is usually measured using the Degree for Angle. Note that the value of Prandtl Meyer Function at Downstream Mach no. is always negative.
Can the Prandtl Meyer Function at Downstream Mach no. be negative?
Yes, the Prandtl Meyer Function at Downstream Mach no., measured in Angle can be negative.
What unit is used to measure Prandtl Meyer Function at Downstream Mach no.?
Prandtl Meyer Function at Downstream Mach no. is usually measured using the Degree[°] for Angle. Radian[°], Minute[°], Second[°] are the few other units in which Prandtl Meyer Function at Downstream Mach no. can be measured.
Let Others Know
✖
Facebook
Twitter
Reddit
LinkedIn
Email
WhatsApp
Copied!