Tests on Models of Three British Airplanes in the Variable Density Wind Tunnel (1928)
NASA Technical Reports Server (NTRS) · leaf 25
24 REPORT NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS … 0 .2 .4 -6 .8 10 12 Bristol Fighter airplane model with R. A. F. 30 Cl wings Fig. 24.—Lift/drag vs. lift coefficient. Bristol Fighter air- plane model with R. A. F. 30 wings &0 1.6 1.2 Climax. .8 .4 0\ « 10,000,000 6 1,000,000 z 100,000 Reynolds Number 30 40 50 60 70 60 SO 100 Per cent of chord…
NASA Technical Reports Server (NTRS)
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