Mach Disk of Dual Coaxial Axisymmetric Jets
Author:
Affiliation:
1. Indian Institute of Technology, Madras, India
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference14 articles.
1. Effect of acoustic excitation on the flow over a low- Re airfoil
2. A natural low-frequency oscillation of the flow over an airfoil near stalling conditions
3. Experimental measurements in a large separation bubble due to a simulated glaze ice shape
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