Assessment of Electrically Actuated Redundant Control Surface Layouts for a Hybrid Wing Body Concept
Author:
Affiliation:
1. Georgia Institute of Technology
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2014-2428
Reference38 articles.
1. 1Maier, R. “ACFA 2020 Summary of Achievements,” Tech. Rep. Deliverable D0.9, EADS Innovation Works, Munich, Germany, Oct. 2012.
2. Conceptual Design of an N+3 Hybrid Wing Body Subsonic Transport
3. A Computational Design Engine for Multi-Disciplinary Optimisation with Application to a Blended Wing Body Configuration
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3. Multidisciplinary Approach to Assessing Actuation Power of a Hybrid Wing–Body;Journal of Aircraft;2016-07
4. Uncertainty Quantification for the Actuation Power Requirements of a Hybrid Wing Body Configuration with Electrically Actuated Flight Control Surfaces;53rd AIAA Aerospace Sciences Meeting;2015-01-03
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