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  • Zur Berechnung der laminaren Reibungsschicht bei Überschallgeschwindigkeit

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.

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Original:
Abhandlungen der Braunschweigischen Wissenschaftlichen Gesellschaft Band 3, 1951, S. 239-264
Date Issued:
1951
DOI:
10.24355/dbbs.084-201212061103-0
URN:
urn:nbn:de:gbv:084-12120611033
Language:
German
Type of Resource:
Text
Extent:
27 S.
Place Term:
Braunschweig
Publisher:
Vieweg
Keywords:
  1. Brunsvicensien der Universitätsbibliothek Braunschweig
    Typ
    Schlagwort
  1. Abhandlungen der BWG
    Typ
    Schlagwort
DDC:
620 Ingenieurwissenschaften
URL:
http://www.digibib.tu-bs.de/?docid=00046236
Library shelfmark::
BWG-1(3)

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