TY  - JOUR
AB  - MUCH has been said earlier concerning the scale effect on drag. A few words must be added on the scale effect on lift near the stall, for it is here that ordinary small‐scale wind tunnel tests may be very misleading. The curves of Fig. 9 show the maximum lift coefficient of two wing sections plotted against Reynolds number, and the difference of behaviour is at once apparent.
VL  - 8
IS  - 7
SN  - 0002-2667
DO  - 10.1108/eb030066
UR  - https://doi.org/10.1108/eb030066
AU  - Relf E.F.
PY  - 1936
Y1  - 1936/01/01
TI  - Aeronautical Progress 1930–1936: A Review of Scientific Progress Given in the James Forrest Lecture
T2  - Aircraft Engineering and Aerospace Technology
PB  - MCB UP Ltd
SP  - 185
EP  - 193
Y2  - 2024/04/25
ER  -