By T. C. Wittenberg, T. J. van Baten, A. de Boer
Plane layout four (2001) 99–113
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Additional resources for Design of fiber metal laminate shear panels for ultra-high capacity aircraft
Example text
A McDonnell Douglas F-15C of the 433rd Fighter Weapons School pulls away from its tanker before beginning its role in a Red Flag “Large Force Employment Exercise”. Not only was the Eagle designed to be technically superior to all other fighters of its day, but the USAF’s constant and intense training programs – especially those flown over the Nevada desert environment – forged in its pilots the proficiency needed to beat any of them. (USAF) CHRONOLOGY 1961 February 16 Secretary of Defense (SecDef) Robert McNamara directs the USAF and US Navy to develop a single aircraft to satisfy the requirements for both the USAF’s tactical strike mission and the US Navy’s fleet air defense mission, giving birth to the ill-fated, joint-service Tactical Fighter Experimental (TFX) program.
Adding the plumbing, pneumatics, and electrical connections to carry CFTs allowed an additional 9,800lbs of fuel to be carried and gave the fully loaded Eagle an endurance of 5 hrs 20 min. This permitted the F-15C to fly 1,060 miles into contested airspace, patrol/fight for 20 minutes, and return with a 30-minute fuel reserve, all without air-to-air refueling. The first F-15C flew on February 26, 1979, the new variant being appreciably more effective in the air-to-air role than the A-model Eagle.
In February 1965, Lt Col John W. Bohn Jr wrote a position paper arguing for a “high-low mix” tactical air force, where a few dedicated high performance (and high-tech) air-to-air fighters – placing emphasis on maneuverability instead of speed – would achieve aerial superiority, allowing a host of “low tech” (and low-cost) fighter-bombers to fulfill their missions with impunity. The position was endorsed by Gen John P. ” Two-and-a-half years later, in July 1967, the Soviets unveiling their newest fighter – a massive twin-jet, twin-tail interceptor with singularly stunning performance – suddenly gave rise to a renewed, urgent, and increased impetus to the USAF’s development of an F-4 replacement.
Design of fiber metal laminate shear panels for ultra-high capacity aircraft by T. C. Wittenberg, T. J. van Baten, A. de Boer
by Anthony
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