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Numerical Simulations of Inviscid Supersonic and Hypersonic Flows.

紀錄類型:	書目-電子資源 : Monograph/item
正題名/作者:	Numerical Simulations of Inviscid Supersonic and Hypersonic Flows./
作者:	Han, Ryan Mathew.
出版者:	Ann Arbor : ProQuest Dissertations & Theses, : 2020,
面頁冊數:	82 p.
附註:	Source: Masters Abstracts International, Volume: 82-06.
Contained By:	Masters Abstracts International82-06.
標題:	Aerospace engineering. -
電子資源:	http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=28093587
ISBN:	9798698525363

Numerical Simulations of Inviscid Supersonic and Hypersonic Flows.
Han, Ryan Mathew.

Numerical Simulations of Inviscid Supersonic and Hypersonic Flows. - Ann Arbor : ProQuest Dissertations & Theses, 2020 - 82 p.

Source: Masters Abstracts International, Volume: 82-06.

Thesis (M.S.)--University of California, Davis, 2020.

This item must not be sold to any third party vendors.

With the always advancing aviation and space industries, supersonic and hypersonic flows are continually becoming more important to model and understand. Inviscid, compressible fluid mechanics are described by systems of hyperbolic partial differential equations, which are used in this thesis to model various supersonic and hypersonic flows. These flows include those through a converging-diverging nozzle, over a two dimensional wedge, over a cone, and over airfoils. Various flow phenomena such as normal, bow, oblique, and fishtail shocks are correctly modeled and shown. Through analysis of the results, it is found that each of the models in this paper demonstrate the correct qualitative flow characteristics for each set of boundary conditions. Accurate data for normal and attached shocks, including the shock position, shock angle, and post-shock flow conditions, as well as accurate expansion fan pressures are found and verified with various publications, all while using very simple numerical methods which are easy to implement and program.

ISBN: 9798698525363Subjects--Topical Terms:

1002622
Aerospace engineering.
Subjects--Index Terms:

Computational fluid dynamics

Numerical Simulations of Inviscid Supersonic and Hypersonic Flows.
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245 1 0 $a Numerical Simulations of Inviscid Supersonic and Hypersonic Flows.
260 1 $a Ann Arbor : $b ProQuest Dissertations & Theses, $c 2020
300 $a 82 p.
500 $a Source: Masters Abstracts International, Volume: 82-06.
500 $a Advisor: Hafez, Mohamed.
502 $a Thesis (M.S.)--University of California, Davis, 2020.
506 $a This item must not be sold to any third party vendors.
520 $a With the always advancing aviation and space industries, supersonic and hypersonic flows are continually becoming more important to model and understand. Inviscid, compressible fluid mechanics are described by systems of hyperbolic partial differential equations, which are used in this thesis to model various supersonic and hypersonic flows. These flows include those through a converging-diverging nozzle, over a two dimensional wedge, over a cone, and over airfoils. Various flow phenomena such as normal, bow, oblique, and fishtail shocks are correctly modeled and shown. Through analysis of the results, it is found that each of the models in this paper demonstrate the correct qualitative flow characteristics for each set of boundary conditions. Accurate data for normal and attached shocks, including the shock position, shock angle, and post-shock flow conditions, as well as accurate expansion fan pressures are found and verified with various publications, all while using very simple numerical methods which are easy to implement and program.
590 $a School code: 0029.
650 4 $a Aerospace engineering. $3 1002622
650 4 $a Mechanical engineering. $3 649730
650 4 $a Fluid mechanics. $3 528155
653 $a Computational fluid dynamics
653 $a Inviscid
653 $a Numerical simulation
653 $a Shocks
690 $a 0538
690 $a 0548
690 $a 0204
710 2 $a University of California, Davis. $b Mechanical and Aerospace Engineering. $3 3190211
773 0 $t Masters Abstracts International $g 82-06.
790 $a 0029
791 $a M.S.
792 $a 2020
793 $a English
856 4 0 $u http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=28093587