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 12
11 AIRFOIL TESTS IN FOUR OPEN WIND TUNNEL JETS OF DIFFERENT SHAPES … Figure J2.—2 to l circular side jet with seaplane model set-up next caUbrated for several speeds against the integrated TESTS mean dynamic pressure at the model position. Preliminary calibration tests were necessary after Alignment tests were then made in each jet to de- the installation of each…
NASA Technical Reports Server (NTRS)
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