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In February 1976, work commenced to automate the methods contained in the USAF Stability and Control DATCOM, specifically those contained in sections 4, 5, 6 and 7.The work was performed by the McDonnell Douglas Corporation under contract with the United States Air Force in conjunction with engineers at the Air Force Flight Dynamics Laboratory in Wright-Patterson Air Force Base.
The Spitfire wing may be classified as: "a conventional low-wing cantilever monoplane with unswept elliptical wings of moderate aspect ratio and slight dihedral".. The wing configuration or planform of a fixed-wing aircraft (including both gliders and powered aeroplanes) is its arrangement of lifting and related surfaces.
Aircraft wing configurations are one of the major aspects of an aircraft's design and are a primary feature in aircraft recognition. Subcategories This category has the following 16 subcategories, out of 16 total.
The Maneuvering Characteristics Augmentation System (MCAS) is a flight stabilizing feature developed by Boeing that became notorious for its role in two fatal accidents of the 737 MAX in 2018 and 2019, which killed all 346 passengers and crew among both flights.
The company developed its own aircraft design software, Advanced Aircraft Analysis (AAA), as well as a second design program for a NASA Small Business Innovative Research contract. [ 5 ] In 2002 he published Roskam's Airplane War Stories a collection of stories about airplane design and analysis and engineering mistakes that were made.
Software updates planned for Boeing Inc.’s troubled 737 Max 8 aircraft, grounded worldwide after two deadly crashes, may not be enough to satisfy critics.
Composite aircraft allow the individual components to continue flying independantly - OTOH the top wing of the slip wing would have glided/crashed to the ground after release and lacked any controls (no ailerons, flaps or even a vertical stabilizer) - not the same as the Pemberton Billing "slip wing" which were just another name for a parasite ...
The X-53 Active Aeroelastic Wing (AAW) development program is a completed American research project that was undertaken jointly by the Air Force Research Laboratory (AFRL), Boeing Phantom Works and NASA's Dryden Flight Research Center, where the technology was flight tested on a modified McDonnell Douglas F/A-18 Hornet.