TY  - RPRT
TI  - A comparison of the spanwise loading calculated by various methods with experimental loadings obtained on a 45 degrees sweptback wing of aspect ratio 8 at a Reynolds number of 4.0 x 10(exp 6)
AU  - Schneider, William C
PY  - 1952
UR  - https://ntrs.nasa.gov/citations/19930086685
ID  - 19930086685
ER  -