572516 N616NA Underwing Supersonic Cruise Exhaust Nozzles.jpg 572516 N616NA Underwing Supersonic Cruise Exhaust NozzlesThumbnails572516 Propulsion Nozzle Wind Tunnel572516 N616NA Underwing Supersonic Cruise Exhaust NozzlesThumbnails572516 Propulsion Nozzle Wind Tunnel572516 N616NA Underwing Supersonic Cruise Exhaust NozzlesThumbnails572516 Propulsion Nozzle Wind Tunnel572516 N616NA Underwing Supersonic Cruise Exhaust NozzlesThumbnails572516 Propulsion Nozzle Wind Tunnel572516 N616NA Underwing Supersonic Cruise Exhaust NozzlesThumbnails572516 Propulsion Nozzle Wind Tunnel572516 N616NA Underwing Supersonic Cruise Exhaust NozzlesThumbnails572516 Propulsion Nozzle Wind Tunnel572516 N616NA Underwing Supersonic Cruise Exhaust NozzlesThumbnails572516 Propulsion Nozzle Wind Tunnel
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). Test nozzle during Transonic Speeds Research in this 1969 photo of the trimotor test-bed F-106. Photo via Earle Boyer taken by J. David Clinton.
Facebook
Information
Author
NASA Glenn Research Center J. David Clinton
Rating score
no rate
Rate this photo
Visits
910
Dimensions
2048*1402
File
572516 N616NA Underwing Supersonic Cruise Exhaust Nozzles.jpg
Filesize
732 KB
Powered by Piwigo
© F-106DeltaDart.com Founded 1998. All Rights Reserved