Characterization of Unsteady Flow Structures Near Leading-Edge Slat: Part I: PIV Measurements
Author:
Affiliation:
1. NASA Langley Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2004-2801
Reference44 articles.
1. 1Khorrami, M. R.,Singer, B. A.,and Lockard, D.P. "Time-AccurateSimulations and AcousticAnalysis ofSlat Free-Shear-Layer: Part II,"AIAAPaper 2002-2579,2002.
2. 2Choudhari, M., Khorrami, M. R., Lockard, D. P., Atkins, H., and Lilley, G. "Slat Cove Noise Modeling: A Posteriori Analysis ofUnsteadyRANS Simulations,"AIAAPaper 2002-2468, 2002.
3. 3Dobryzynski, W., Nagakura, K, Gehlhar, B., and Buschbaum, A. "Airframe NoiseStudies on Wings with Deployed High-Lift Devices," AIAAPaper 1998-2337,1998.
4. Measurements of Reynolds stress profiles on a high-lift airfoil
5. 5Storms, B. L., Hayes, J. A., Moriarty, P. J., and Ross, J.C. "Aeroacoustic Measurements of Slat Noise on a Three-Dimensional High-Lift System", AIAAPaper 99-1957,1999.
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