NASA Technical Reports Server (NTRS) 19790011883: Inverse boundary-layer technique for airfoil designReport as inadecuate



 NASA Technical Reports Server (NTRS) 19790011883: Inverse boundary-layer technique for airfoil design


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A description is presented of a technique for the optimization of airfoil pressure distributions using an interactive inverse boundary-layer program. This program allows the user to determine quickly a near-optimum subsonic pressure distribution which meets his requirements for lift, drag, and pitching moment at the desired flow conditions. The met

Author: NASA Technical Reports Server (NTRS)

Source: https://archive.org/







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