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Numerical Simulations of High-Speed ...

Greene, Patrick Timothy.

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Numerical Simulations of High-Speed Flows Over Complex Geometries.

Record Type:	Electronic resources : Monograph/item
Title/Author:	Numerical Simulations of High-Speed Flows Over Complex Geometries./
Author:	Greene, Patrick Timothy.
Description:	139 p.
Notes:	Source: Dissertation Abstracts International, Volume: 75-08(E), Section: B.
Contained By:	Dissertation Abstracts International75-08B(E).
Subject:	Engineering, Aerospace. -
Online resource:	http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=3613959
ISBN:	9781303782930

Numerical Simulations of High-Speed Flows Over Complex Geometries.
Greene, Patrick Timothy.

Numerical Simulations of High-Speed Flows Over Complex Geometries. - 139 p.

Source: Dissertation Abstracts International, Volume: 75-08(E), Section: B.

Thesis (Ph.D.)--University of California, Los Angeles, 2014.

The effects of surface roughness on the stability of hypersonic flow are of great importance to hypersonic vehicles. Surface roughness can greatly alter boundary-layer flow and cause transition to turbulence to occur much earlier compared to a smooth wall, which will result in a significant increase of wall heating and skin friction drag. The work presented in this dissertation was motivated by a desire to study the effects of isolated roughness elements on the stability of hypersonic boundary layers. A new code was developed which can perform high-order direct numerical simulations of high-speed flows over arbitrary geometries. A fifth-order hybrid weighted essentially non-oscillatory scheme was implemented to capture any steep gradients in the flow created by the geometries. The simulations are carried out on Cartesian grids with the geometries imposed by a third-order cut-cell method. A multi-zone refinement method is also implemented to provide extra resolution at locations with expected complex physics. The combination results in a globally fourth-order scheme.

ISBN: 9781303782930Subjects--Topical Terms:

1018395
Engineering, Aerospace.

Numerical Simulations of High-Speed Flows Over Complex Geometries.
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100 1 $a Greene, Patrick Timothy. $3 3169121
245 1 0 $a Numerical Simulations of High-Speed Flows Over Complex Geometries.
300 $a 139 p.
500 $a Source: Dissertation Abstracts International, Volume: 75-08(E), Section: B.
500 $a Advisers: John Kim; Jeff D. Eldredge.
502 $a Thesis (Ph.D.)--University of California, Los Angeles, 2014.
520 $a The effects of surface roughness on the stability of hypersonic flow are of great importance to hypersonic vehicles. Surface roughness can greatly alter boundary-layer flow and cause transition to turbulence to occur much earlier compared to a smooth wall, which will result in a significant increase of wall heating and skin friction drag. The work presented in this dissertation was motivated by a desire to study the effects of isolated roughness elements on the stability of hypersonic boundary layers. A new code was developed which can perform high-order direct numerical simulations of high-speed flows over arbitrary geometries. A fifth-order hybrid weighted essentially non-oscillatory scheme was implemented to capture any steep gradients in the flow created by the geometries. The simulations are carried out on Cartesian grids with the geometries imposed by a third-order cut-cell method. A multi-zone refinement method is also implemented to provide extra resolution at locations with expected complex physics. The combination results in a globally fourth-order scheme.
520 $a Results for two-dimensional and three-dimensional test cases show good agreement with previous results and will be presented. Results confirming the code's high order of convergence will also be shown. Two-dimensional simulations of flow over complex geometries will be presented to demonstrate the code's capabilities. Results for Mach 6 flow over a three-dimensional cylindrical roughness element will also be presented. The results will show that the code is a promising tool for the study of hypersonic roughness-induced transition.
590 $a School code: 0031.
650 4 $a Engineering, Aerospace. $3 1018395
650 4 $a Applied Mathematics. $3 1669109
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710 2 $a University of California, Los Angeles. $b Aerospace Engineering 0279. $3 2092189
773 0 $t Dissertation Abstracts International $g 75-08B(E).
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791 $a Ph.D.
792 $a 2014
793 $a English
856 4 0 $u http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=3613959