Maintenance window scheduled to begin at February 14th 2200 est. until 0400 est. February 15th

(e.g. yourname@email.com)

Forgot Password?

    Defense Visual Information Distribution Service Logo

    11-Inch High Speed Tunnel

    Issued by: on

    VIRIN:
    Date Created:
    City:
    State:
    Country:
    11-Inch High Speed Tunnel

    WASHINGTON, DISTRICT OF COLUMBIA, UNITED STATES

    09.23.2009

    Courtesy Photo

    NASA

    Drawing of balance for 11-Inch High Speed Tunnel. The 11-Inch HST used compressed air from the Variable-Density Tunnel (when it was being depressurized). It was similar to a venturi-type wind tunnel. Without a model, air flow speeds approached Mach 1. One of the unique features of this tunnel was its automatic-recording balance used to measure the forces. John Stack supplied a general description of the balance in NACA TR No. 463 (pp. 401-403). "The balance must measure the large range of forces resulting from the wide speed range over which tests are made, and it must be automatic recording because the allowable time for observations is short. The balance measures the lift, drag, and pitching moment by multiplying and recording the deflection of steel springs (cantilever beam type) to which the forces are transmitted. The essential parts consist of a cast-iron cradle in which is mounted a yoke to which the model is attached, the linkages necessary to transmit the forces to the steel springs, and a camera for multiplying and recording the deflections of the springs.

    NASA Identifier: L5509

    IMAGE INFO

    Date Taken: 09.23.2009
    Date Posted: 10.17.2012 14:05
    Photo ID: 727565
    Resolution: 1536x1313
    Size: 229.75 KB
    Location: WASHINGTON, DISTRICT OF COLUMBIA, US

    Web Views: 4
    Downloads: 0

    PUBLIC DOMAIN