TY  - RPRT
TI  - Automated design optimization of supersonic airplane wing structures under dynamic constraints.
AU  - Fox, R. L.
AU  - Miura, H.
AU  - Rao, S. S.
PY  - 1972
UR  - https://ntrs.nasa.gov/citations/19720041702
ID  - 19720041702
ER  -