TY  - RPRT
TI  - Numerical method for predicting unsteady aerodynamic loadings caused by control surface motions in subsonic flow.
AU  - Rowe, W. S.
AU  - Winther, B. A.
AU  - Redman, M. C.
PY  - 1973
UR  - https://ntrs.nasa.gov/citations/19730040744
ID  - 19730040744
ER  -