TY  - RPRT
TI  - Results of differential elevon/aileron deflection for lateral control optimization and elevon hinge moment investigations on an 0.015-scale model (49-0) of the space shuttle orbiter in the NASA/Langley Research Center 8 foot TPT (OA116)
AU  - Lindsey, A. I.
AU  - Milam, M. D.
PY  - 1974
UR  - https://ntrs.nasa.gov/citations/19750007652
ID  - 19750007652
ER  -