DTIC ADA041583: Iterative Calculation of Flow Past a Thick Cambered Wing Near the Ground,Report as inadecuate



 DTIC ADA041583: Iterative Calculation of Flow Past a Thick Cambered Wing Near the Ground,


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A method to compute the steady low-speed inviscid flow past a wing in free air, is extended to take account of ground effect. The basic method represents the perturbation due to the wing by iteratively computed distributions of sources and doublets on the wing chordal surface; at each iteration the ground effect is represented by the images in the

Author: Defense Technical Information Center

Source: https://archive.org/



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