TY  - RPRT
TI  - Development of a structural optimization capability for the aeroelastic tailoring of composite rotor blades with straight and swept tips
AU  - Friedmann, P. P.
AU  - Venkatesan, C.
AU  - Yuan, K.
PY  - 1992
UR  - https://ntrs.nasa.gov/citations/19930036373
ID  - 19930036373
ER  -