F8U-3 stick modifications - Stick controls in studio.
F8U-3 stick modifications
Crusader on runway. Navy aircraft number 6340. L59-6101 caption:  The Navy's Vought XF8U-3 Supersonic Fighter was an entirely new design as compared to the earlier F8U Crusader series. This jet plane lost in competition with the McDonnell F4H, however, and was never put into production. Langley used the XF8U-3 in some of the first flight measurements of sonic boom intensity.  Photograph published in Engineer in Charge A History of the Langley Aeronautical Laboratory, 1917-1958 by James R. Hansen. Page 507. Caption:  Chance Vought F8U-3 airplane used in sonic boom investigation at Wallops, June-August 1959.  Photograph published in A New Dimension  Wallops Island Flight Test Range: The First Fifteen Years by Joseph Shortal. A NASA publication. Page 672.
F8U-3 aircraft
Crusader on runway. Navy aircraft number 6340. L59-6101 caption:  The Navy's Vought XF8U-3 Supersonic Fighter was an entirely new design as compared to the earlier F8U Crusader series. This jet plane lost in competition with the McDonnell F4H, however, and was never put into production. Langley used the XF8U-3 in some of the first flight measurements of sonic boom intensity.  Photograph published in Engineer in Charge A History of the Langley Aeronautical Laboratory, 1917-1958 by James R. Hansen. Page 507. Caption:  Chance Vought F8U-3 airplane used in sonic boom investigation at Wallops, June-August 1959.  Photograph published in A New Dimension  Wallops Island Flight Test Range: The First Fifteen Years by Joseph Shortal. A NASA publication. Page 672.
F8U-3 aircraft
Wings for large scale model aircraft.
F8U-3 wing model Vought
Views of F-8U Crusader Aircraft at NASA Langley
Views of F8U Airplane
Pieces of small scale model broken in 16 Foot Transonic Tunnel.
Broken F8U-3 model
Views of F-8U Crusader Aircraft at NASA Langley
Views of F8U Airplane
Exhaust cone damage.
Damaged tail cone on F8U-3
L57-660 A technician prepares dynamic models of the Bell X-1E and the Vought XF-8U Crusader for wind tunnel testing in 1957. The Crusader was then the Navy's fastest aircraft- maximum speed Mach 1.75 at 35,000 Feet. Photograph published in Engineer in Charge: A History of the Langley Aeronautical Laboratory, 1917-1958 by James R. Hansen. Page 307.
Bell X-1E and Vought XF-8U Dynamic Models in 1957