259.jpg 572516 N616NA Underwing PropulsionThumbnails572516 N616NA Underwing Supersonic Cruise Exhaust Nozzles572516 N616NA Underwing PropulsionThumbnails572516 N616NA Underwing Supersonic Cruise Exhaust Nozzles572516 N616NA Underwing PropulsionThumbnails572516 N616NA Underwing Supersonic Cruise Exhaust Nozzles572516 N616NA Underwing PropulsionThumbnails572516 N616NA Underwing Supersonic Cruise Exhaust Nozzles572516 N616NA Underwing PropulsionThumbnails572516 N616NA Underwing Supersonic Cruise Exhaust Nozzles572516 N616NA Underwing PropulsionThumbnails572516 N616NA Underwing Supersonic Cruise Exhaust Nozzles572516 N616NA Underwing PropulsionThumbnails572516 N616NA Underwing Supersonic Cruise Exhaust Nozzles
F-106B 57-2516, NASA ID No. N616NA of the NASA Lewis Research Center, Cleveland OH (NASA N816NA at Langley Research Center, Hampton VA) in 1968 during a test flight of Underwing Supersonic Cruise Exhaust Nozzles during Transonic Speeds Research. Two 25 inch diameter J85 nacelles designed to contain the J85-GE-13 afterburning turbojet engines. The left wing engine had a Research Inlet and Research Exhaust Nozzle, while the right wing engine was for Reference with an open inlet and cylindrical nozzle. [NASA via Earle Boyer collection]
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