3-D LDV measurements over a delta wing in pitch-up motion
Author:
Affiliation:
1. Virginia PolytechnicInst. and State Univ., Blacksburg
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1993-185
Reference11 articles.
1. '2. Rediniotis, 0. K. "The Transient Development of Vortices Over a Delta Wing,' Ph.D. Dissertation, VPI & SU.October 1992.
2. Leading-edge vortices due to low Reynolds number flow past a pitching delta wing
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1. Numerical investigation of an advanced aircraft model during pitching motion at high incidence;Science China Technological Sciences;2015-10-28
2. Asymptotic behavior of solutions of the renormalization group k-epsilon turbulence model;AIAA Journal;1994-05
3. Crossflow topology of vortical flows;AIAA Journal;1994-05
4. Flow control over delta wings at high angles of attack;11th Applied Aerodynamics Conference;1993-08-09
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