In Spring 1927, while Spirit of St. Louis was being built by Ryan Airline Company in San Diego, Charles Lindbergh corresponded with the Standard Steel Propeller Company of Pittsburgh regarding the best pitch setting for its ground-adjustable propeller blades.
The aluminum-alloy blades were off-the-shelf items, using a Clark Y airfoil and a twist distribution suitable for Ryan’s mail planes, upon which the design of Spirit was based. The Clark Y was a profile commonly used for propeller blades, not because it had any special aerodynamic advantage but because its flat bottom made fabricating blades and measuring their pitch angles easier.
Because the propeller’s pitch could not be changed in flight, Lindbergh had a ticklish decision to make. He could pitch the prop for best efficiency in cruise, but it would then be less suitable for takeoff; or he could pitch it for maximum takeoff thrust and give up some range. The airplane would weigh around 5,100 pounds and have a static thrust of around 700 pounds. It was not going to leap forward in any case. The runway at New York’s Roosevelt Field, where the flight would begin, was 5,000 feet long, with telephone lines just beyond the departure end. The takeoff for the Paris flight would be the airplane’s first at maximum weight. For it to not succeed would be fatal to not only the project but possibly the pilot as well.
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Esta historia es de la edición September 2020 de Flying.
Comience su prueba gratuita de Magzter GOLD de 7 días para acceder a miles de historias premium seleccionadas y a más de 9,000 revistas y periódicos.
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