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- W135398969 abstract "The computer code for an advanced dynamic airfoil model (ADAM) is described. The code is capable of calculating steady or unsteady flow over two-dimensional airfoils with allowances for boundary layer separation. Specific types of airfoil motions currently installed are steady rectilinear motion, impulsively started rectilinear motion, constant rate pitching, sinusoidal pitch oscillations, sinusoidal lateral plunging, and simulated Darrieus turbine motion. Other types of airfoil motion may be analyzed through simple modifications of a single subroutine. The code has a built-in capability to generate the geometric parameters for a cylinder, the NACA four-digit series of airfoils, and a NASA NLF-0416 laminar airfoil. Other types of airfoils are easily incorporated. The code ADAM is currently in a state of development. It is theoretically consistent and complete. However, further work is needed on the numerical implementation of the method." @default.
- W135398969 created "2016-06-24" @default.
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- W135398969 date "1987-06-01" @default.
- W135398969 modified "2023-09-27" @default.
- W135398969 title "User's manual for ADAM (Advanced Dynamic Airfoil Model)" @default.
- W135398969 hasPublicationYear "1987" @default.
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