Effects of Reduced Frequency on the Behaviors of Burst Point Around a Pitching Double Delta Wing
Author:
Publisher
Springer Singapore
Link
http://link.springer.com/content/pdf/10.1007/978-981-10-7542-1_8
Reference9 articles.
1. Ericsson LE (1996) Pitch rate effects on delta wing vortex breakdown. J Aircraft 33(3):639–642
2. Gritskevich MS et al (2012) Development of DDES and IDDES formulations for the k-ω shear stress transport model. Flow Turbul Combust 88:431–449
3. Gursul I (2000) Proposed mechanism for time lag of vortex breakdown location in unsteady flows. J Aircraft 37(4):733–736
4. Gursul I (2005) Review of unsteady vortex flows over slender delta wings. J Aircraft 42(2):299–319
5. Liu J et al (2016) Vortex breakdown flows around a double-delta wing during pitching motion based on DDES. In 6th Symposium on Hybrid RANS-LES Methods, Sept. 26–28, Strasbourg, France
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