Conference Proceedings

Aerodynamic optimization of subsonic flying wing configurations

20th AIAA Applied Aerodynamics Conference (2002)
DOI: 10.2514/6.2002-2931
43Citations
Citations of this article
37Readers
Mendeley users who have this article in their library.
Get full text

Abstract

The paper presents some aerodynamic results of initial design studies carried out at ONERA and Airbus France, on flying wing configurations. A description of the analysis and the design process, using CFD tools, is given and some results regarding the effects of the planform are presented. © 2002 by ONERA.

Cite

CITATION STYLE

APA

Mialon, B., Fol, T., & Bonnaud, C. (2002). Aerodynamic optimization of subsonic flying wing configurations. In 20th AIAA Applied Aerodynamics Conference. American Institute of Aeronautics and Astronautics Inc. https://doi.org/10.2514/6.2002-2931

Register to see more suggestions

Mendeley helps you to discover research relevant for your work.

Already have an account?

Save time finding and organizing research with Mendeley

Sign up for free