Theoretical evaluation of a V/STOL fighter model utilizing the PAN AIR code

@inproceedings{Howell1982TheoreticalEO,
  title={Theoretical evaluation of a V/STOL fighter model utilizing the PAN AIR code},
  author={George A. Howell and Ishwar C Bhateley},
  year={1982}
}
The PAN AIR computer code was investigated as a tool for predicting closely coupled aerodynamic and propulsive flowfields of arbitrary configurations. The NASA/Ames V/STOL fighter model, a configuration of complex geometry, was analyzed with the PAN AIR code. A successful solution for this configuration was obtained when the nozzle exit was treated as an impermeable surface and no wakes were included around the nozzle exit. When separated flow was simulated from the end of the nacelle… CONTINUE READING