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Unsteady Flow Characteristics of a N...
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Sorrell, Michael D.,
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Unsteady Flow Characteristics of a Normal Shock Wave and Associated Lambda Foot /
紀錄類型:
書目-電子資源 : Monograph/item
正題名/作者:
Unsteady Flow Characteristics of a Normal Shock Wave and Associated Lambda Foot // Michael D Sorrell.
作者:
Sorrell, Michael D.,
面頁冊數:
1 electronic resource (151 pages)
附註:
Source: Masters Abstracts International, Volume: 85-10.
Contained By:
Masters Abstracts International85-10.
標題:
Aerospace engineering. -
電子資源:
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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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.
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