TY  - RPRT
TI  - An efficient method for computing unsteady transonic aerodynamics of swept wings with control surfaces
AU  - Liu, D. D.
AU  - Kao, Y. F.
AU  - Fung, K. Y.
PY  - 1989
UR  - https://ntrs.nasa.gov/citations/19890009870
ID  - 19890009870
ER  -