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Experimental Determination of Jet Boundary Corrections for Airfoil Tests in Four Open Wind Tunnel Jets of Different Shapes (1931)
NASA Technical Reports Server (NTRS) · leaf 6
— 76- 4" — {a3.267m) -ft a" … A—Spherical honeycomb (i2" X 2H" ± conical G—Airfoil, inverted. TV—Micro-manometer. H—Counterweight wire boot and wire. tubes), bellmouth of beaver board. O—Drag balance. B—Honeycomb-fine (3" X W tubes). I—Counterweight. P—Lift and moment wire boots. C—Service pi tot tube. J—Ceiling. Q—Entrance…NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
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