Machine calculation of compressible laminar boundary layers
- 1 April 1965
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 3 (4) , 639-647
- https://doi.org/10.2514/3.2940
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- SOLUTION OF THE GENERAL BOUNDARY-LAYER EQUATIONS FOR COMPRESSIBLE LAMINAR FLOW, INCLUDING TRANSVERSE CURVATUREPublished by Defense Technical Information Center (DTIC) ,1963
- The Numerical Treatment of Differential EquationsPublished by Springer Nature ,1960