Vortex-dominated flow with viscous core structure
Author:
Affiliation:
1. NASA, Langley Research Center, Hampton, VA
2. Aachen, Rheinisch-Westfaelische Technische Hochschule, West Germany
3. New York University, NY
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1985-1556
Reference73 articles.
1. AIM Professional Study Series,1971
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1. Far-field turbulent vortex-wake/exhaust plume interaction for subsonic and HSCT airplanes;Fluid Dynamics Conference;1996-06-17
2. Navier-Stokes calculation of wing wake structure;12th Applied Aerodynamics Conference;1994-06-20
3. Increasing and decreasing the stability of a confined vortex by forcing;23rd Fluid Dynamics, Plasmadynamics, and Lasers Conference;1993-07-06
4. On the dynamics of near-wall turbulence;Philosophical Transactions of the Royal Society of London. Series A: Physical and Engineering Sciences;1991-08-15
5. Navier-Stokes computation of flow around a round-edged double-delta wing;AIAA Journal;1990-06
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