Decay of Fluctuating Wall-Pressure Field of Mach 5 Turbulent Boundary Layer
Author:
Affiliation:
1. University of Texas at Austin, Austin, Texas 78712-1085
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.837
Reference28 articles.
1. Power- and cross-spectra and space-time correlations of surface fluctuating pressures at Mach numbers between 1.6 and 2.5
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3. Mean and fluctuating flow measurements of a fully-developed, non-adiabatic, hypersonic boundary layer
4. A comparison of the turbulence structure of subsonic and supersonic boundary layers
5. The Physics of Supersonic Turbulent Boundary Layers
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1. Velocimetry Measurements of Unstart of an Inlet-Isolator Model in Mach 5 Flow;AIAA Journal;2010-09
2. Cavity Oscillation Mechanisms in High-Speed Flows;AIAA Journal;2004-10
3. Time-Series Analysis of Supersonic Base-Pressure Fluctuations;AIAA Journal;2004-03
4. Time-Series Analysis of Supersonic Base-Pressure Fluctuations;33rd AIAA Fluid Dynamics Conference and Exhibit;2003-06-23
5. Relationship Between Upstream Turbulent Boundary-Layer Velocity Fluctuations and Separation Shock Unsteadiness;AIAA Journal;2002-12
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