TY  - RPRT
TI  - A parametric study of supersonic laminar flow for swept wings using linear stability analysis
AU  - Cummings, Russell M.
AU  - Garcia, Joseph A.
AU  - Tu, Eugene L.
PY  - 1995
UR  - https://ntrs.nasa.gov/citations/19960016110
ID  - 19960016110
ER  -