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Receptivity and Forced Response to Acoustic Disturbances in High-Speed Boundary Layers
P Balakumar1, Rudolph A King1, Amanda Chou1
1NASA Langley Research Center, Hampton, Virginia 23681.
Summary
Supersonic boundary-layer receptivity was studied using Navier-Stokes equations. Acoustic disturbances amplified within the boundary layer, with amplitudes up to 2.5 times larger than the incoming field.
Area of Science:
- Fluid Dynamics
- Aerodynamics
- Acoustics
Background:
- Supersonic boundary layers are sensitive to freestream disturbances.
- Understanding receptivity is crucial for predicting flow behavior and performance.
Purpose of the Study:
- Investigate supersonic boundary-layer receptivity to acoustic disturbances.
- Analyze the generation and amplification of perturbations within the boundary layer.
Main Methods:
- Solved Navier-Stokes equations for Mach 3.5 flow over a cone.
- Generated freestream acoustic disturbances using a wavy nozzle wall.
- Utilized linearized Euler equations to model acoustic radiation.
Main Results:
- Oblique impingement of acoustic disturbances did not generate noticeable instability modes.
- Boundary layer perturbations were a direct response to external acoustic forcing.
- Amplification factors of 2.5 and 1.5 were observed for zero and large azimuthal wave numbers, respectively.
Conclusions:
- The supersonic boundary layer exhibits forced response to acoustic disturbances.
- The amplitude of internal perturbations significantly exceeds the incoming acoustic field.
- Azimuthal wave number influences the amplification of forced disturbances.
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