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- The trend for decreasing the drag of aircraft is retention of laminar flow in the boundary layer over a large portion of the surface. The laminar boundary layer was studied in a low turbulence wind tunnel for low subsonic velocities. The method used and results of measurements of very low levels of turbulence are presented. Measurements were performed by a constant-resistance thermoanemometer.
- NASA Technical Reports Server (NTRS) Collection.
- Document ID: 19780018162.
Accession ID: 78N26105.
- No Copyright.
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