NASA Technical Reports Server (NTRS) : A pdf

NASA Technical Reports Server (NTRS) : A

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Description of the Book:

A computer program written in a table “”look-up” format, is presented which provides a comprehensive data base on NACA 16-series airfoils. The geometry covered is limited to cambers for a design-lift coefficient from 0.0 to 0.7 and thickness ratios from 4 to 21%. The data include Mach numbers from 0.3 to 1.6, angles of attack from -4 to 8 degrees, and lift coefficients from 0.0 to 0.8. Extrapolation is used to obtain data from Mach numbers, angles of attack, and lift coefficients beyond those for which data are available. A routine to adjust the lift and drag coefficients beyond stall is included. The uses and limitations of the program are also discussed

• Creator/s: NASA Technical Reports Server (NTRS
• Date: 9/1/1983
• Year: 1983
• Book Topics/Themes: NASA Technical Reports Server (NTRS), AERODYNAMIC CHARACTERISTICS, AIRFOILS, COMPUTER PROGRAMS, INTERPOLATION, ANGLE OF ATTACK, CAMBER, MACH NUMBER, PROGRAM VERIFICATION (COMPUTERS), PROPELLERS, TURBOPROP AIRCRAFT, Maksymiuk, C. M., Watson, S. A

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