@misc{indiciae0c0929949aec,
  title = {Flow field analysis of aircraft configurations using a numerical solution to the three-dimensional unified supersonic/hypersonic small-disturbance equations, part 2},
  author = {Dsylva, E.},
  year = {1972},
  url = {https://ntrs.nasa.gov/citations/19720009558},
  note = {Source identifier: 19720009558}
}