VORTEX BREAKDOWN DUE TO FLAPS ON A 60$^{\circ}$DELTA WING- BODY

  • Gopinath, N. (National Trisonic Aerodynamic Facilities National Aerospace Laboratories) ;
  • Sridharan, R. (National Trisonic Aerodynamic Facilities National Aerospace Laboratories)
  • Published : 2008.08.17