Accession Number : AD0694393

Title :   DEVICE FOR INVESTIGATING THE FLOW IN A WIND TUNNEL,

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s) : Zhustrin,K. V. ; Sitnikov,V. P.

Report Date : 25 APR 1969

Pagination or Media Count : 5

Abstract : The device consists of pressure pickups mounted on a probe which, in turn, is mounted on a movable rod. The device also has an electromechanical drive, and a rigid pneumometric line leading into the housings of the rod and the support. To increase efficiency, the device is provided with a flexible pneumometric line connecting the outlets of the rigid pneumometric line located at the end of the movable rod and the upper part of the support; the flexible line is mounted on a rigid stand which assumes a given configuration when the rod is displaced. (Author)

Descriptors :   (*WIND TUNNELS, GAS FLOW), (*GAS FLOW, INSTRUMENTATION), PATENTS, USSR

Subject Categories : Aerodynamics
      Test Facilities, Equipment and Methods
      Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE