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    Construction of a 2- by 2-foot transonic adaptive-wall test section at the NASA Ames Research Center (1986)
    In:  Other Sources
    Details
    Publication Date: 2019-06-28
    Description: The development of a new production-size, two-dimensional, adaptive-wall test section with ventilated walls at the NASA Ames Research Center is described. The new facility incorporates rapid closed-loop operation, computer/sensor integration, and on-line interference assessment and wall corrections. Air flow through the test section is controlled by a series of plenum compartments and three-way slide vales. A fast-scan laser velocimeter was built to measure velocity boundary conditions for the interference assessment scheme. A 15.2-cm- (6.0-in.-) chord NACA 0012 airfoil model will be used in the first experiments during calibration of the facility.
    Keywords: RESEARCH AND SUPPORT FACILITIES (AIR)
    Type: AIAA PAPER 86-1089
    Format: text
    Location Call Number Expected Availability
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    NASA TECHNICAL REPORTS
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