Effect of Compressibility on Normal-force, Pressure, and Load Characteristics of a Tapered Wing of NACA 66-series Airfoil Sections with Split Flaps
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Flat-plate flaps with no wing cutouts and flaps having Clark Y sections with corresponding cutouts made in wing were tested for various flap deflections, chord-wise locations, and gaps between flaps and airfoil contour. The drag was slightly lower for wing with airfoil section flaps. Satisfactory aileron effectiveness was obtained with flap gap of 20% wing chord and flap-nose location of 80 percent wing chord behind leading edge. Airflow was smooth and buffeting negligible.
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A frequency tripler has been developed using an integrated planar back-to-back -n-n(sup +) varactor device in a waveguide mount at 220 GHz.
Observations made from Kitt Peak, Arizona, of the 233.9 GHz emission line of 18 0 16 0 in the upper stratosphere and lower mesosphere are reported.
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