Prandtl–Meyer function
id:
prandtl-meyer-function-320-1389179
title:
Prandtl–Meyer function
text:
In aerodynamics, the Prandtl–Meyer function describes the angle through which a flow turns isentropically from sonic velocity (M=1) to a Mach (M) number greater than 1. The maximum angle through which a sonic flow can be turned around a convex corner is calculated for M = ∞ . For an ideal gas, it is expressed as follows, where ν is the Prandtl–Meyer function, M is the Mach number of the flow and γ is the ratio of the specific heat capacities. By convention, the constant of integration is selecte
brand slug:
wiki
category slug:
encyclopedia
description:
original url:
https://en.wikipedia.org/wiki/Prandtl%E2%80%93Meyer_function
date created:
date modified:
2023-07-27T09:24:24Z
main entity:
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image:
{"content_url":"https://upload.wikimedia.org/wikipedia/commons/f/f4/Prandtl_meyer_function.png","width":1212,"height":825}
fields total:
13
integrity:
14