Experimental study of flow field distribution over a generic cranked double delta wing
Author:
Publisher
Elsevier BV
Subject
Mechanical Engineering,Aerospace Engineering
Reference27 articles.
1. A comparative study of two UCAV type wing planforms—performance and stability considerations;Nangia;Aeronaut J,2006
2. Flying wings, a new paradigm for civil aviation;Martinez-Val;Acta Polytech,2007
3. Unsteady aerodynamics of non-slender delta wings;Gursul;Prog Aerosp Sci,2005
4. Luckring J. A survey of factors affecting blunt leading-edge separation for swept and semi slender wings. 28th AIAA applied aerodynamics conference. Reston: AIAA; 2010. p. 1–34.
5. Implications of scale effect for the prediction of high angle of attack aerodynamics;Munro;Prog Aerosp Sci,2005
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