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Multi-Mode Instabilities Arising in ...

Liang, Tony,

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Multi-Mode Instabilities Arising in Hypersonic Flow Conditions for Aerospace Applications /

Record Type:	Electronic resources : Monograph/item
Title/Author:	Multi-Mode Instabilities Arising in Hypersonic Flow Conditions for Aerospace Applications // Tony Liang.
Author:	Liang, Tony,
Description:	1 electronic resource (131 pages)
Notes:	Source: Dissertations Abstracts International, Volume: 85-08, Section: B.
Contained By:	Dissertations Abstracts International85-08B.
Subject:	Mechanical engineering. -
Online resource:	https://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=30988383
ISBN:	9798381722215

Multi-Mode Instabilities Arising in Hypersonic Flow Conditions for Aerospace Applications /
Liang, Tony,

Multi-Mode Instabilities Arising in Hypersonic Flow Conditions for Aerospace Applications /Tony Liang. - 1 electronic resource (131 pages)

Source: Dissertations Abstracts International, Volume: 85-08, Section: B.

Research in hypersonic aerodynamics is important in understanding the practicality of sustained high-speed flight and the design parameters of such vehicles. Hypersonic boundary layer transition is dominated by the presence of various disturbance (Mack) modes present within the boundary layer which undergo modal growth and eventually transition the flow to turbulence. Understanding the dynamics of these modes and their interactions within the boundary layer can bridge the knowledge gaps in the fundamental causes of heat transfer, friction drag, lift and other properties which become critically important in hypersonic flight.The aim of this research is to perform an analytical study utilizing computational fluid dynamics (CFD) coupled with boundary layer stability analysis employing linear stability theory (LST) and parabolized stability equations (PSE) to help understand the dynamics of Mack modes and their nonlinear interactions. One question to be studied is the source of energy driving the 1st and 2nd mode instabilities. A characterization of the energetics of the 1st and 2nd modes was performed at various flow conditions to further understand physical mechanisms governing the modal growth pathway to transition, and was shown that the traditional 1st mode definition is incomplete. A design study into a geometry conducive to 1st and 2nd mode interactions was performed and investigated. With such a geometry, the dynamics between a 1st mode dominated boundary layer with an existing 2nd mode was investigated. Finally, with understanding of the thermoacoustic interpretation of the 2nd mode, a impedance boundary condition is applied to a canonical conical geometry in an attempt to analyze its effect on certain unstable waves within the boundary layer. Understanding the dynamics of these modes and their interactions within the boundary layer can bridge fundamental knowledge gaps governing various phenomena in hypersonic flight.

English

ISBN: 9798381722215Subjects--Topical Terms:

649730
Mechanical engineering.
Subjects--Index Terms:

Boundary layer transition

Multi-Mode Instabilities Arising in Hypersonic Flow Conditions for Aerospace Applications /
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264 1 $a Ann Arbor : $b ProQuest Dissertations & Theses, $c 2024
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500 $a Advisors: Kuehl, Joseph J. Committee members: Prasad, Ajay; Veron, Fabrice; Van Buren, Tyler.
502 $b Ph.D. $c University of Delaware $d 2024.
520 $a Research in hypersonic aerodynamics is important in understanding the practicality of sustained high-speed flight and the design parameters of such vehicles. Hypersonic boundary layer transition is dominated by the presence of various disturbance (Mack) modes present within the boundary layer which undergo modal growth and eventually transition the flow to turbulence. Understanding the dynamics of these modes and their interactions within the boundary layer can bridge the knowledge gaps in the fundamental causes of heat transfer, friction drag, lift and other properties which become critically important in hypersonic flight.The aim of this research is to perform an analytical study utilizing computational fluid dynamics (CFD) coupled with boundary layer stability analysis employing linear stability theory (LST) and parabolized stability equations (PSE) to help understand the dynamics of Mack modes and their nonlinear interactions. One question to be studied is the source of energy driving the 1st and 2nd mode instabilities. A characterization of the energetics of the 1st and 2nd modes was performed at various flow conditions to further understand physical mechanisms governing the modal growth pathway to transition, and was shown that the traditional 1st mode definition is incomplete. A design study into a geometry conducive to 1st and 2nd mode interactions was performed and investigated. With such a geometry, the dynamics between a 1st mode dominated boundary layer with an existing 2nd mode was investigated. Finally, with understanding of the thermoacoustic interpretation of the 2nd mode, a impedance boundary condition is applied to a canonical conical geometry in an attempt to analyze its effect on certain unstable waves within the boundary layer. Understanding the dynamics of these modes and their interactions within the boundary layer can bridge fundamental knowledge gaps governing various phenomena in hypersonic flight.
546 $a English
590 $a School code: 0060
650 4 $a Mechanical engineering. $3 649730
650 4 $a Aerospace engineering. $3 1002622
650 4 $a Fluid mechanics. $3 528155
653 $a Boundary layer transition
653 $a Hypersonic flight
653 $a Parabolized stability equations
653 $a Linear stability theory
653 $a Computational fluid dynamics
690 $a 0548
690 $a 0538
690 $a 0204
710 2 $a University of Delaware. $b Mechanical Engineering. $e degree granting institution. $3 3829855
720 1 $a Kuehl, Joseph J. $e degree supervisor.
773 0 $t Dissertations Abstracts International $g 85-08B.
790 $a 0060
791 $a Ph.D.
792 $a 2024
856 4 0 $u https://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=30988383