Efficient infinite-swept wing solver for steady and unsteady compressible flows
Author:
Funder
Royal Academy of Engineering
Engineering and Physical Sciences Research Council
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference25 articles.
1. Modeling and simulating aircraft stability and control – the SimSAC project;Rizzi;Prog. Aerosp. Sci.,2011
2. Development of a multilevel multidisciplinary-optimization capability for an industrial environment;Piperni;AIAA J.,2013
3. Uncertainty Quantification & Management in High Value Manufacturing Special Interest Group;Butchers,2015
4. Adaptive design of experiments for efficient and accurate estimation of aerodynamic loads;Da Ronch;Aircr. Eng. Aerosp. Technol.,2017
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