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Finite Wing
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FILE INFORMATION
Ranked as 26993 on our all-time top downloads list with 2173 downloads.
Ranked as 3930 on our top downloads list for the past seven days with 4 downloads.
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finitewing.zip
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Filename
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finitewing.zip (Download)
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Title
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Finite Wing
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Description
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"Finite Wing" (wing.89p) uses Glauert's method (1926) to analyze finite wings with linear taper and linear washout. The solution references “Mechanics of Flight, 2nd ed.” (Warren F. Phillips, 2010). Inputs include: Number of Fourier coefficients, N; Span, b (units length); Taper ratio, R_t; Aspect ratio, R_a 3-D lift coefficient, Cl; Sectional zero-lift angle of attack, a_L0s (degrees); Maximum washout, O (degrees). Outputs include: Lift curve slope, Cl_a (per radian); Induced drag coefficient, Cd_i; Root angle of attack, root_a (degrees); Zero-lift angle of attack, a_L0 (degrees); Span efficiency factor, e_s; Kappa values (k_L, epsilon_Omega, k_D, k_DL, k_DO).
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Author
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Robert Nordlund (bnordlund+ticalc@gmail.com)
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Category
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TI-89 BASIC Science Programs (Applied Physics, Engineering)
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File Size
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3,213 bytes
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File Date and Time
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Sun Apr 10 15:34:44 2011
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Documentation Included?
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Yes
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