Support Interference Computations of Forced Oscillation Test for a Flying-Wing Dynamic Model
Author:
Publisher
Springer Singapore
Link
http://link.springer.com/content/pdf/10.1007/978-981-13-3305-7_28
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4. Sherer SE, Visbal MR, Gordnier RE (2009) Computational study of Reynolds number and angle-of-attack effects on a 1303 UCAV configuration with a high-order overset-Mesh algorithm, AIAA 2009-751
5. Tomac M, Rizzi A, Nangia RK et al (2010) Engineering methods on the SACCON configuration - Some design considerations, AIAA 2010-4398
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