Wind-tunnel investigation of air inlet and outlet openings on a streamline body
Description:
In connection with the general problem of providing air flow to an aircraft power plant located within a fuselage, an investigation was conducted in the Langley 8-foot high-speed tunnel to determine the effect on external drag and pressure distribution of air inlet openings located at the nose of a streamline body. Air outlet openings located at the tail and at the 21-percent and 63-percent stations of the body were also investigated. Boundary layer transition measurements were made and correla…
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Date:
September 11, 1940
Creator:
Becker, John V.
Item Type:
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Report
Partner:
UNT Libraries Government Documents Department