The measurement of skin friction in a turbulent boundary layer at a Mach number of 2.5, including the effect of a shock-wave
- 6 November 1952
- journal article
- Published by The Royal Society in Proceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences
- Vol. 215 (1120), 84-99
- https://doi.org/10.1098/rspa.1952.0198