DTIC ADA052621: Dominance of Radiated Aerodynamic Noise on Boundary-Layer Transition in Supersonic-Hypersonic Wind Tunnels. Theory and ApplicationReport as inadecuate



 DTIC ADA052621: Dominance of Radiated Aerodynamic Noise on Boundary-Layer Transition in Supersonic-Hypersonic Wind Tunnels. Theory and Application


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An experimental investigation was conducted to determine the effects of radiated aerodynamic-noise on boundary-layer transition in supersonic- hypersonic wind tunnels. It is conclusively shown that the aerodynamic noise (pressure fluctuations associated with sound waves), which radiate from the tunnel wall, turbulent boundary layer, will dominate t

Author: Defense Technical Information Center

Source: https://archive.org/







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