An Approximate Method for the Calculation of the Laminar and Turbulent Boundary Layer by Simple Quadrature for Two-Dimensional and Axially Symmetric Flow
- 1 June 1952
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 19 (6) , 428-429
- https://doi.org/10.2514/8.2325
Abstract
No abstract availableKeywords
This publication has 5 references indexed in Scilit:
- On Supersonic Flow of a Two-Dimensional Jet in Uniform StreamJournal of the Aeronautical Sciences, 1952
- Beitrag zur Berechnung der turbulenten GrenzschichtenArchive of Applied Mechanics, 1951
- Untersuchungen über konvergente und divergente, turbulente ReibungsschichtenArchive of Applied Mechanics, 1943
- Die turbulente Reibungsschicht in ebener Strömung bei Druckabfall und DruckanstiegArchive of Applied Mechanics, 1931
- Zur näherungsweisen Integration der Differentialgleichung der Iaminaren GrenzschichtZAMM - Journal of Applied Mathematics and Mechanics / Zeitschrift für Angewandte Mathematik und Mechanik, 1921