NASA Technical Reports Server (NTRS) 19810021544: Comparisons of AEROX computer program predictions of lift and induced drag with flight test dataReport as inadecuate



 NASA Technical Reports Server (NTRS) 19810021544: Comparisons of AEROX computer program predictions of lift and induced drag with flight test data


NASA Technical Reports Server (NTRS) 19810021544: Comparisons of AEROX computer program predictions of lift and induced drag with flight test data - Download this document for free, or read online. Document in PDF available to download.

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The AEROX aerodynamic computer program which provides accurate predictions of induced drag and trim drag for the full angle of attack range and for Mach numbers from 0.4 to 3.0 is described. This capability is demonstrated comparing flight test data and AEROX predictions for 17 different tactical aircraft. Values of minimum (skin friction, pressure

Author: NASA Technical Reports Server (NTRS)

Source: https://archive.org/







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