TY  - RPRT
TI  - A comparison of the spanwise loading calculated by various methods with experimental loadings obtained on a 45 degree sweptback wing of aspect ratio 8.02 at a Reynolds number of 4.0 x 10(6)
AU  - Schneider, Willaim C
PY  - 1954
UR  - https://ntrs.nasa.gov/citations/19930092218
ID  - 19930092218
ER  -