Please use this identifier to cite or link to this item: http://hdl.handle.net/10397/93034
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Title: Reverse design of ultrasonic absorptive coating for the stabilization of mack modes
Authors: Tian, X 
Zhao, R
Long, T 
Wen, CY 
Issue Date: Jun-2019
Source: AIAA journal, June 2019, v. 57, no. 6, p. 2264-2269
Abstract: The effects of ultrasonic absorptive coating (UAC) admittance on the first and second modes in a high-speed boundary layer are analyzed using linear stability theory. It is shown that the growth rate of the first mode is increased as UAC admittance phase θ varies from 0.5π to π, whereas the second mode is amplified when θ tends to 0.5π and damped if θ ≥ 0.75π. The frequency range of the first mode is broadened when θ is in the vicinity of π, and the second mode shifts to low frequencies when θ < π. Moreover, the stabilization or destabilization effects on Mack modes, frequency band broadening, and frequency shifting are promoted by large UAC admittance magnitudes. Based on the requirements of the admittance phase and magnitude for the stabilization of Mack modes, a design strategy for UAC is proposed to stabilize the second mode in a wide frequency range with the first mode little amplified.
Keywords: Compressible boundary layer
Freestream mach number
Thermal protection system
Flow conditions
Temperature ratio
Flow velocity
Angle of attack
Navier stokes equations
Hypersonic transports
Collocation method
Publisher: American Institute of Aeronautics and Astronautics
Journal: AIAA journal 
ISSN: 0001-1452
EISSN: 1533-385X
DOI: 10.2514/1.J058105
Rights: Copyright © 2019 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.
This is the peer reviewed version of the following article: Tian, X., Zhao, R., Long, T., & Wen, C. Y. (2019). Reverse design of ultrasonic absorptive coating for the stabilization of Mack modes. AIAA Journal, 57(6), 2264-2269, which has been published in final form at https://doi.org/10.2514/1.J058105.
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