TY  - RPRT
TI  - A new, improved method for separating turbulent boundary layer for aerodynamic performance prediction of trailing edge stall airfoils
AU  - Goradia, S.
AU  - Morgan, H. L., Jr.
PY  - 1986
UR  - https://ntrs.nasa.gov/citations/19860064852
ID  - 19860064852
ER  -