Modeling of Controlled Shock-Wave/Boundary-Layer Interactions in Transonic Channel Flow
Author:
Affiliation:
1. ONERA, 92190 Meudon, France
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.1267
Reference22 articles.
1. Passive drag reduction on a complete NACA 0012 airfoil at transonic Mach numbers
2. EUROSHOCK - Drag Reduction by Passive Shock Control
3. Experimental study of mesoflaps for SBLI control
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2. Response of an oblique shock train to downstream periodic pressure perturbations;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2017-09-07
3. Adaptive Control of Shock Waves with a Passively Morphing Layer for Rotating Blades;Journal of Aerospace Engineering;2015-03
4. Experimental and numerical study of forced shock-wave oscillations in a transonic channel;Aerospace Science and Technology;2006-05
5. Experimental and Numerical Study of Forced Shock-Wave Oscillations in a Transonic Channel;33rd AIAA Fluid Dynamics Conference and Exhibit;2003-06-23
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