TY  - RPRT
TI  - Shock capturing finite-difference and characteristic reference plane techniques for the prediction of three-dimensional nozzle-exhaust flowfields
AU  - Dash, S.
AU  - Delguidice, P.
PY  - 1978
UR  - https://ntrs.nasa.gov/citations/19780017412
ID  - 19780017412
ER  -