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Preliminary wing model tests in the variable density wind tunnel of the National Advisory Committee for Aeronautics (1926)

NASA Technical Reports Server (NTRS) · leaf 8

An illustration from Preliminary wing model tests in the variable density wind tunnel of the National Advisory Committee for Aeronautics, 1926, leaf 8 — 211 PEELIMI1TAST WBXQ MODEL TESTS … ao -at -02 -a3 -0.4 -as -as -a? &(abouf quarter chord) Fro. 17.—Test No. 57-3. Tank pressure 8.2 atmospheres. Dyitamlo pressure Fro. 18.—TestNo.87-t Tank pressure 18.44 atmospheres. Dynamic pressure g=258 kg/m'. Reynolds Number 1,490,000 ?=531 ke/m» Reynolds Number 2,880,000

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