TY  - RPRT
TI  - A method for predicting the low speed chordwise pressure distribution over sharp edge airfoil sections with plain flaps at the leading and trailing edges
AU  - Nuber, Robert J
AU  - Cahill, Jones F
PY  - 1950
UR  - https://ntrs.nasa.gov/citations/19930086336
ID  - 19930086336
ER  -