@misc{indiciaee25e16a0693f,
  title = {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)},
  author = {Lindsey, A. I. and Milam, M. D.},
  year = {1974},
  url = {https://ntrs.nasa.gov/citations/19750007652},
  note = {Source identifier: 19750007652}
}