Measuring and testing – Wind tunnel: aerodynamic wing and propeller study
Patent
1979-12-18
1982-01-12
Yasich, Daniel M.
Measuring and testing
Wind tunnel: aerodynamic wing and propeller study
73190H, 73340, G01K 1706, G01M 900
Patent
active
043099017
ABSTRACT:
A heat transfer calibration plate for use in obtaining data for determining the heat transfer coefficient in a wind tunnel test system having a copper plate mounted in an aluminum support plate. Nine heat flux gages are positioned in a horizontal and a vertical row with a center gage common to the two rows. A heater is provided to heat the plate to the desired temperature. Thermocouples are provided to indicate plate temperature. Outputs of the thermocouples and heat flux gages are recorded on a recorder. All of the heat flux gages except the center gage are connected to the recorder through a rotary switch. Plenum temperature and pressure are also recorded.
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Laub Bernard
Rolinski Edmund J.
Killoren Richard J.
Singer Donald J.
The United States of America as represented by the Secretary of
Yasich Daniel M.
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