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The Custer CCW-5 was a twin-engined, 5-seat aircraft of pusher configuration, which used a channel wing claimed to enable low speed flight and short take-offs. Two CCW-5s flew, eleven years apart, but the type never entered production. The aircraft was the third and last of a series of Custer Channel Wing designs.
The prototype Custer CCW-1 single-seat test aircraft displayed at the National Air and Space Museum facility at Silver Hill, Maryland in April 1982 Channel Wing concept testing at Langley The first aircraft to incorporate Custer's concept was the CCW-1 which was fitted with a single-seat and was powered by two 75 horsepower (56 kW) Lycoming O ...
Channel Wing aircraft CCW-5. The channel wing is an aircraft wing principle developed by Willard Ray Custer in the 1920s. The most important part of the wing consists of a half-tube with an engine placed in the middle, driving a propeller placed at the rear end of the channel formed by the half-tube. Antonov Izdeliye 181 Experimental
In 1939 Custer founded the National Aircraft Corporation and, on November 12, 1942, started development of the CCW-1 (CusterChannelWing 1) experimental aircraft. With the CCW-2 that followed, he could achieve almost vertical starts, and flight almost like a helicopter. The military started a number of trials which were subsequently canceled ...
This is a list of aircraft in the collection of the Pima Air & Space Museum in Tucson, Arizona. The identity of an aircraft may be its civil registration or its military serial number. An aircraft may have had civil use following its retirement from the military; furthermore an aircraft may not be displayed with the same identification as is ...
A circulation control wing (CCW) is a form of high-lift device for use on the main wing of an aircraft to increase the maximum lift coefficient and reduce the stalling speed. CCW technology has been in the research and development phase for over sixty years. Blown flaps were an early example of CCW. [1]
Production at a rate of one aircraft per month was planned for the B-290. [3] The Brigadier was chosen by Willard Ray Custer as the basis of his Custer CCW-5, which used the fuselage and tail of the Brigadier, but had a modified wing with the engines sitting in U-shaped ducts, [7] but other than the two CCW-5s no production of the B-290 ...
On 21 May 1947, the wing was activated by Air Defense Command (ADC) as the 505th Aircraft Control and Warning Group, drawing on the personnel and assets of the former 412th Air Force Base Unit. Stationed at McChord Field it become the first of ADC's post-World War II aircraft control and warning units.
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