Hydrodynamic Tunnel Test Of Concorde

UNITED KINGDOM - DECEMBER 01: In 1959 the Supersonic Transport Aircraft Committee recommended the construction of a fleet of long range intercontinental airliners which would fly almost twice as high and over twice as fast as those in service at that time; at Mach 2.0, twice the speed of sound. In 1962, the British and French Governments signed an agreement to develop the aircraft together. Exhaustive testing using a range of models was carried out in order to ascertain the ideal shape for the aircraft, and it became clear that a narrow delta wing would have sufficiently low drag for high-speed cruising and still have good handling characteristics at low speed and landing. (Photo by SSPL/Getty Images)
UNITED KINGDOM - DECEMBER 01: In 1959 the Supersonic Transport Aircraft Committee recommended the construction of a fleet of long range intercontinental airliners which would fly almost twice as high and over twice as fast as those in service at that time; at Mach 2.0, twice the speed of sound. In 1962, the British and French Governments signed an agreement to develop the aircraft together. Exhaustive testing using a range of models was carried out in order to ascertain the ideal shape for the aircraft, and it became clear that a narrow delta wing would have sufficiently low drag for high-speed cruising and still have good handling characteristics at low speed and landing. (Photo by SSPL/Getty Images)
Hydrodynamic Tunnel Test Of Concorde
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Editorial #:
90745197
Collection:
SSPL
Date created:
January 01, 1965
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Release info:
Not released. More information
Source:
SSPL
Object name:
10307891
Max file size:
3504 x 2767 px (11.68 x 9.22 in) - 300 dpi - 2 MB