Yaw-control efficiency analysis for a diamond wing configuration with outboard split flaps

Author:

Pfnür StefanORCID,Oppelt Sven,Breitsamter Christian

Publisher

Springer Science and Business Media LLC

Subject

Aerospace Engineering,Transportation

Reference24 articles.

1. Airbus Defence and Space: Successful first flight for UAV demonstrator SAGITTA (Press Release) (2017). https://www.airbus.com/newsroom/press-releases/en/2017/07/successful-first-flight-for-uav-demonstrator-sagitta.html . Accessed 26 July 2018

2. Allmaras, S.R., Johnson, F.T., Spalart, P.R.: Modifications and clarifications for the implementation of the Spalart–Allmaras turbulence model. In: 7th International Conference on Computational Fluid Dynamics, Big Island (HI), United States, ICCFD7-1902 (2012)

3. Begin, L.: The Northrop flying wing prototypes. In: Aircraft Prototype and Technology Demonstrator Symposium, Meeting Paper Archive, Dayton (OH), AIAA Paper 1983-1047 (1983). https://doi.org/10.2514/6.1983-1047

4. Bourding, P., Gatto, A., Friswell, M.I.: Potential of articulated split wingtips for morphing-based control of a flying wing. In: 25th Applied Aerodynamics Conference, Miami (FL), AIAA Paper 2007-4443 (2007). https://doi.org/10.2514/6.2007-4443

5. Burns, B.R.A.: Design considerations for the satisfactory stability and control of military combat aeroplanes. In: AGARD Specialists’ Meeting on “Stability and Control”, Braunschweig, Germany, April 10–13, 1972, no. 119 in AGARD Conference Proceedings

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