Zur laminaren Grenzschicht am schiebenden Zylinder Teil I
- 1 October 1952
- journal article
- Published by Springer Nature in Archiv der Mathematik
- Vol. 3 (3) , 216-231
- https://doi.org/10.1007/bf01899366
Abstract
No abstract availableKeywords
This publication has 12 references indexed in Scilit:
- Simplified Laminar Boundary-Layer Calculations for Bodies of Revolution and for Yawed Wings - ErrataJournal of the Aeronautical Sciences, 1952
- Grenzschichten an zylindrischen Körpern mit nichtstationärer QuerbewegungZAMM - Journal of Applied Mathematics and Mechanics / Zeitschrift für Angewandte Mathematik und Mechanik, 1952
- The Profile Drag of Yawed Wings of Infinite SpanAeronautical Quarterly, 1951
- On the Calculation of the Rate of Heat Transfer Through a Laminar Boundary LayerJournal of the Aeronautical Sciences, 1951
- The Laminar Boundary Layer on a Rotating BladeJournal of the Aeronautical Sciences, 1951
- The boundary layer of a class of infinite yawed cylindersMathematical Proceedings of the Cambridge Philosophical Society, 1950
- A Theoretical Investigation of Heat Transfer in the Laminar Flow Regions of AirfoilsJournal of the Aeronautical Sciences, 1950
- The Boundary Layer of Yawed Infinite WingsJournal of the Aeronautical Sciences, 1949
- Ein Differenzenverfahren zur Berechnung laminarer GrenzschichtenArchive of Applied Mechanics, 1948
- The Boundary Layer of Yawed CylindersJournal of the Aeronautical Sciences, 1948