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Airfoil Section Characteristics as Affected by Variations of the Reynolds Number (1937)
NASA Technical Reports Server (NTRS) · leaf 13
,000 .ft ,07 8 > 41,700 M 06 6 0 o 05 4 I' 04 Hi I- 0% 03 .02 .01 0 .4 !-./ .2 .2 Airfoil: N.A.C.A. 4415 8 .Size. 5,'x30" Ve/.(ft./sec.):69 Pres. fsthd. aim.): 1/4 to 20 Airfoil: N.A.C.A. 44/5 Test: V. D.T.I I S3 Dote: 8-34 Dote: 8-34 Test: V.D.T. 1163 -.4 ' Where tesfed: L.M.A.L. Results… … 1.6 1.8 .2 .4 .6 .8 1.0 1.2 1.4 -12 - 8 -4 0 4 8 12 16 20 24 28 -.4 es) Angle of attach for infinite aspect ratio, aQ (degrt Lift coefficient, CL Figure 11—N. A. C. A. 8318.NASA Technical Reports Server (NTRS)
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