TY  - RPRT
TI  - A computer program for wing subsonic aerodynamic performance estimates including attainable thrust and vortex lift effects
AU  - Carlson, H. W.
AU  - Walkley, K. B.
PY  - 1982
UR  - https://ntrs.nasa.gov/citations/19820011277
ID  - 19820011277
ER  -