[ stop the slideshow ]

572516 Underwing Propulsion Nozzle 1

5895/13357
3740.jpg 572516 Underwing Propulsion Nozzle 00Thumbnails572516 Underwing Propulsion Nozzle 2572516 Underwing Propulsion Nozzle 00Thumbnails572516 Underwing Propulsion Nozzle 2572516 Underwing Propulsion Nozzle 00Thumbnails572516 Underwing Propulsion Nozzle 2572516 Underwing Propulsion Nozzle 00Thumbnails572516 Underwing Propulsion Nozzle 2572516 Underwing Propulsion Nozzle 00Thumbnails572516 Underwing Propulsion Nozzle 2572516 Underwing Propulsion Nozzle 00Thumbnails572516 Underwing Propulsion Nozzle 2572516 Underwing Propulsion Nozzle 00Thumbnails572516 Underwing Propulsion Nozzle 2

F-106B 57-2516, NASA ID No. N616NA of the NASA Lewis Research Center, Cleveland OH (NASA N816NA while at Langley Research Center, Hampton VA). I [Earle Boyer] do not recall the particulars of all the nozzles and inlets flown during Transonic Speeds Research but this one is referred to as a Spike Inlet. [NASA via Earle Boyer collection]