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Titlebook: Aerodynamic Drag Reduction Technologies; Proceedings of the C Peter Thiede Conference proceedings 2001 Springer-Verlag Berlin Heidelberg 20

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https://doi.org/10.1007/978-3-322-81101-1 the European Community A nacelle . has been defined for the CFM56-5C engine installed on the A340. The Hybrid Laminar Flow nacelle features a translating forebody replacing both the intake and the fan cowl doors and also an upgraded thrust reverser. The major conclusion of the multidisciplinary wor
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https://doi.org/10.1007/978-3-322-89083-2sign methods, is described. The evaluation of the aerodynamic design of three wing configurations by wind-tunnel model testing is described. Results are presented for independent CFD analyses of the optimised wing configurations, and a comparative analysis of results from design, model test and CFD
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Aerodynamic Drag Reduction Technologies978-3-540-45359-8Series ISSN 1612-2909 Series E-ISSN 1860-0824
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978-3-642-07541-4Springer-Verlag Berlin Heidelberg 2001
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