TY  - RPRT
TI  - Steady and unsteady aerodynamic forces from the SOUSSA surface-panel method for a fighter wing with tip missile and comparison with experiment and PANAIR
AU  - Cunningham, Herbert J.
PY  - 1987
UR  - https://ntrs.nasa.gov/citations/19870016599
ID  - 19870016599
ER  -