Ordinates and Theoretical Pressure-distribution Data for NACA 6- and 6A-series Airfoil Sections with Thicknesses from 2 to 21 and from 2 to 15 Percent Chord, Respectively

Ordinates and Theoretical Pressure-distribution Data for NACA 6- and 6A-series Airfoil Sections with Thicknesses from 2 to 21 and from 2 to 15 Percent Chord, Respectively
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Total Pages : 92
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ISBN-10 : UIUC:30112106632141
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Rating : 4/5 (41 Downloads)

Book Synopsis Ordinates and Theoretical Pressure-distribution Data for NACA 6- and 6A-series Airfoil Sections with Thicknesses from 2 to 21 and from 2 to 15 Percent Chord, Respectively by : Elizabeth W. Patterson

Download or read book Ordinates and Theoretical Pressure-distribution Data for NACA 6- and 6A-series Airfoil Sections with Thicknesses from 2 to 21 and from 2 to 15 Percent Chord, Respectively written by Elizabeth W. Patterson and published by . This book was released on 1961 with total page 92 pages. Available in PDF, EPUB and Kindle. Book excerpt: Summary: Basic thickness forms of the NACA 63-, 64-, 65- series and NACA 63A-, 64A-, 65 A-series airfoil sections are tabulated for thicknesses of 2, 3, 4, and 5 percent chord. Also presented for these thin airfoil sections are theoretical values of pressures and velocity ratios required to obtain theoretical airfoil pressure distributions. In addition, for each family of airfoil sections, cross plots are presented from which ordinates and pressure distributions can be easily obtained for airfoil sections of thicknesses intermediate to those presented in this report, in NACA Report 824 (from 6 to 21 percent chord for the NACA 6-series), and in NACA Report 903 (from 6 to 15 percent chord for the NACA 6A-series).


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