Actuator energy and drag minimization of a blended-wing-body with variable-camber continuous trailing-edge flaps

Author:

Zhao Wei1ORCID,Kapania Rakesh K.1

Affiliation:

1. Kevin T. Crofton Department of Aerospace and Ocean Engineering, Virginia Polytechnic Institute and State University, Blacksburg, USA

Funder

National Aeronautics and Space Administration

Publisher

Informa UK Limited

Subject

Applied Mathematics,Industrial and Manufacturing Engineering,Management Science and Operations Research,Control and Optimization,Computer Science Applications

Reference57 articles.

1. Adegbindin, Moustaine, Nathan Love, Rakesh K. Kapania, and Joseph A. Schetz. 2016. “Control Power Optimization Using Artificial Intelligence for Forward Swept Wing and Hybrid Wing Body Aircraft.” In Proceedings of the 17th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, Paper No. AIAA-2016-3361. Reston, VA: American Institute of Aeronautics and Astronautics. doi:10.2514/6.2016-3361.

2. Blackwell Jr, James A. 1976. “Numerical Method to Calculate the Induced Drag or Optimum Loading for Arbitrary Non-Planar Aircraft.” In Vortex-Lattice Utilization, NASA SP-405. Washington, DC: NASA. doi:http://adsabs.harvard.edu/abs/1976NASSP.405··· 49B.

3. Bonet, John T., Harvey G. Schellenger, Blaine K. Rawdon, Kevin R. Elmer, Sean R. Wakayama, Derrell L. Brown, and Yueping Guo. 2011. “Environmentally Responsible Aviation (ERA) Project N+2 Advanced Vehicle Concepts Study and Conceptual Design of Subscale Test Vehicle (STV) Final Report.” Technical Report NASA/CR-2011-216519, Boeing Research and Technology, Huntington Beach, CA.

4. A methodology for vehicle and mission level comparison of More Electric Aircraft subsystem solutions: Application to the flight control actuation system

5. Analysis of least absolute deviation

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