FLIGHT INVESTIGATION OF INSTALLATION EFFECTS ON A PLUG NOZZLE WITH A SERIES OF BOATTAILED PRIMARY SHROUDS INSTALLED ON AN UNDERLING NACELLE

摘要

Several variations of a boattailed shroud for a 10° conical plug nozzle were tested using an F-106B aircraft for Mach 0.6 to 1.3. The data were obtained so that the tradeoff between boattail and plug size could be studied for an underwing nacelle location. The nozzles were tested with a J85-GE-13 turbojet engine, and the data were compared to previous flight results of installed plug nozzles. Boattail area varied from 31 to 66 percent of the nacelle area. The effect of increasing projected boattail area was to increase the gross thrust coefficient in the same way as from isolated data for flight Mach numbers below 0. 85. The highest gross thrust coefficient (0. 958) was obtained at Mach 0. 95 with a long circular arc shroud configuration with a very small amount of secondary air flow.