TY  - RPRT
TI  - Aerodynamic influence coefficient method using singularity splines.
AU  - Mercer, J. E.
AU  - Weber, J. A.
AU  - Lesferd, E. P.
PY  - 1973
UR  - https://ntrs.nasa.gov/citations/19730032843
ID  - 19730032843
ER  -