Zur Berechnung der laminaren Reibungsschicht bei Überschallgeschwindigkeit

Autor: Schlichting, Hermann
Jazyk: němčina
Rok vydání: 1951
Předmět:
Zdroj: Abhandlungen der Braunschweigischen Wissenschaftlichen Gesellschaft Band 3, 1951, S. 239-264
Popis: 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.
Databáze: OpenAIRE