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Unsteady Flow Characteristics of a N...

Sorrell, Michael D.,

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Unsteady Flow Characteristics of a Normal Shock Wave and Associated Lambda Foot /

Record Type:	Electronic resources : Monograph/item
Title/Author:	Unsteady Flow Characteristics of a Normal Shock Wave and Associated Lambda Foot // Michael D Sorrell.
Author:	Sorrell, Michael D.,
Description:	1 electronic resource (151 pages)
Notes:	Source: Masters Abstracts International, Volume: 85-10.
Contained By:	Masters Abstracts International85-10.
Subject:	Aerospace engineering. -
Online resource:	https://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=30820254
ISBN:	9798382187846

Unsteady Flow Characteristics of a Normal Shock Wave and Associated Lambda Foot /
Sorrell, Michael D.,

Unsteady Flow Characteristics of a Normal Shock Wave and Associated Lambda Foot /Michael D Sorrell. - 1 electronic resource (151 pages)

Source: Masters Abstracts International, Volume: 85-10.

Shock wave interactions are important in a variety of engineering applications, ranging from gas turbines to rocket nozzles. There is much discussion regarding the sources of unsteadiness related to unsteady shock wave structure. This thesis investigates related interactions through spectral analysis of shock wave tracked positions, and instantaneous surface static pressure, temperature, and heat flux. A shadowgraph system for implementing shock wave tracking analysis is employed within a supersonic test section with an inlet freestream Mach number of 1.54. Unsteady surface static pressure and temperature variations are measured at streamwise locations along the bottom wall. Unsteady temperature data are used to determine surface heat flux variations. Pressure, temperature, and heat flux variations are correlated to the position of the normal shock wave through magnitude squared coherence and time lag. Data show complex physical variations that change as frequency, inlet turbulence intensity, and location relative to the shock wave are altered.

English

ISBN: 9798382187846Subjects--Topical Terms:

1002622
Aerospace engineering.
Subjects--Index Terms:

Shock wave

Unsteady Flow Characteristics of a Normal Shock Wave and Associated Lambda Foot /
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100 1 $a Sorrell, Michael D., $e author. $3 3829853
245 1 0 $a Unsteady Flow Characteristics of a Normal Shock Wave and Associated Lambda Foot / $c Michael D Sorrell.
264 1 $a Ann Arbor : $b ProQuest Dissertations & Theses, $c 2024
300 $a 1 electronic resource (151 pages)
336 $a text $b txt $2 rdacontent
337 $a computer $b c $2 rdamedia
338 $a online resource $b cr $2 rdacarrier
500 $a Source: Masters Abstracts International, Volume: 85-10.
500 $a Advisors: Ligrani, Phillip M. Committee members: Hu, Haiyang; Zhang, Guangsheng.
502 $b M.Sc. $c The University of Alabama in Huntsville $d 2024.
520 $a Shock wave interactions are important in a variety of engineering applications, ranging from gas turbines to rocket nozzles. There is much discussion regarding the sources of unsteadiness related to unsteady shock wave structure. This thesis investigates related interactions through spectral analysis of shock wave tracked positions, and instantaneous surface static pressure, temperature, and heat flux. A shadowgraph system for implementing shock wave tracking analysis is employed within a supersonic test section with an inlet freestream Mach number of 1.54. Unsteady surface static pressure and temperature variations are measured at streamwise locations along the bottom wall. Unsteady temperature data are used to determine surface heat flux variations. Pressure, temperature, and heat flux variations are correlated to the position of the normal shock wave through magnitude squared coherence and time lag. Data show complex physical variations that change as frequency, inlet turbulence intensity, and location relative to the shock wave are altered.
546 $a English
590 $a School code: 0278
650 4 $a Aerospace engineering. $3 1002622
650 4 $a Applied physics. $3 3343996
650 4 $a Thermodynamics. $3 517304
650 4 $a Mechanical engineering. $3 649730
653 $a Shock wave
653 $a Rocket nozzles
653 $a Gas turbines
653 $a Shadowgraph system
653 $a Surface heat flux variations
690 $a 0538
690 $a 0548
690 $a 0215
690 $a 0348
710 2 $a The University of Alabama in Huntsville. $b Mechanical and Aerospace Engineering. $e degree granting institution. $3 3825179
720 1 $a Ligrani, Phillip M. $e degree supervisor.
773 0 $t Masters Abstracts International $g 85-10.
790 $a 0278
791 $a M.Sc.
792 $a 2024
856 4 0 $u https://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=30820254