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    Full Scale Wind Tunnel and Seaplane Tow Channel

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    Full Scale Wind Tunnel and Seaplane Tow Channel

    WASHINGTON, DISTRICT OF COLUMBIA, UNITED STATES

    09.23.2009

    Courtesy Photo

    NASA

    Construction progress, studding in Tow Channel office area, Full Scale motor fairing in west exit cone, motor fairing in east exit cone. Propeller and motor fairing for west exit cone. Smith DeFrance described the propellers and motors in NACA TR No. 459. " The propellers are located side by side and 48 feet aft of the throat of the exit-cone bell. The propellers are 35 feet 5 inches in diameter and each consists of four cast aluminum alloy blades screwed into a cast steel hub." "The most commonly used power plant for operating a wind tunnel is a direct-current motor and motor-generator set with Ward Leonard control system. For the full-scale wind tunnel it was found that alternating current slip-ring induction motors, together with satisfactory control equipment, could be purchased for approximately 30 percent less than the direct-current equipment. Two 4,000-horsepower slip-ring induction motors with 24 steps of speed between 75 and 300 r.p.m. were therefore installed. In order to obtain the range of speed one pole change was provided and the other variations are obtained by the introduction of resistance in the rotor circuit. This control permits a variation in air speed from 25 to 118 miles per hour. The two motors are connected through an automatic switchboard to one drum-type controller located in the test chamber. All the control equipment is interlocked and connected through time-limit relays, so that regardless of how fast the controller handle is moved the motors will increase in speed at regular intervals." (p. 294-295)

    NASA Identifier: L5311

    IMAGE INFO

    Date Taken: 09.23.2009
    Date Posted: 10.10.2012 13:36
    Photo ID: 695773
    Resolution: 1138x1536
    Size: 241.45 KB
    Location: WASHINGTON, DISTRICT OF COLUMBIA, US

    Web Views: 23
    Downloads: 1

    PUBLIC DOMAIN