Zur Berechnung der laminaren Reibungsschicht bei Überschallgeschwindigkeit
Recently L. Howarth has given a method to calculate the boundary layer for the velocity distribution and temperature near an insulated wall for compressible laminar flow, the Prandtl number being 1. It is shown here, that approximate solutions of this problem can be obtained in a very simple way by applying the momentum method in the version given by H. Holstein and T. Bohlen for incompressible flow.
Use and reproduction:
All rights reserved