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Concorde's drooping nose, developed by Marshall's of Cambridge, [151] enabled the aircraft to switch from being streamlined to reduce drag and achieve optimal aerodynamic efficiency during flight, to not obstructing the pilot's view during taxi, take-off, and landing operations. Due to the high angle of attack, the long pointed nose obstructed ...
Partial reheat providing a 20% thrust increase [3] was installed to give the take-off thrust required for Concorde to operate from existing runways, and for transonic acceleration from Mach 0.95 up to Mach 1.7; the aircraft flew supersonically without reheat above that speed. At cruise the engine's direct contribution (transferred by its mounts ...
In a pre-computer age, flight engineers were crucial to aviation. Former Concorde flight engineer Warren Hazelby explains how he helped fly the supersonic jet.
For example, Concorde had very high drag (a lift to drag ratio of about 4) at slow speed, but it travelled at high speed for most of the flight. Designers of Concorde spent 5000 hours optimizing the vehicle shape in wind tunnel tests to maximize the overall performance over the entire flightplan.
Five years before Concorde’s first flight, ... The plane would later achieve a speed of just over 2,000 miles per hour, nearly 50% faster than Concorde.
Concorde G-BOAB in storage at London (Heathrow) Airport, following the end of all Concorde flights. G-BOAA (206) first flew on 5 November 1975 from Filton. This aircraft flew with the Red Arrows on 2 June 1996 to celebrate 50 years of Heathrow Airport. It last flew on 12 August 2000 as BA002 from New York JFK to London Heathrow after flying ...
Concorde, the world’s fastest commercial aircraft, has been making a rare journey – floating down New York’s Hudson River. Record-breaking supersonic Concorde airplane floats down New York ...
Afterburning was added to Concorde for take-off to cope with weight increases that came after the initial design. It was also used to accelerate through the high-drag transonic speed range, not because the extra thrust was required, but because it was available and improved the operating economics. The redesigned Tu-144D used engines with no ...