DTIC ADA041585: Iterative Design Techniques for Thick Cambered Wings in Subcritical Flow,Report as inadecuate



 DTIC ADA041585: Iterative Design Techniques for Thick Cambered Wings in Subcritical Flow,


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The author-s method for computing steady, inviscid, subcritical flow past a thick cambered wing is extended to design applications. Four problems are considered: (1) given thickness and doublet (first-order loading) distributions; (2) given thickness and upper-surface pressure distributions; (3) given loading and upper-surface pressure distribution

Author: Defense Technical Information Center

Source: https://archive.org/







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