A Higher-Order Method Implemented in an Unstructured Panel Code to Model Linearized Supersonic Flows

Since their conception in the 1960s, panel codes have remained a critical tool in the design and development of air vehicles. With continued advancement in computational technologies, today's codes are able to solve flow fields around arbitrary bodies more quickly and with higher fidelity than...

Full description

Bibliographic Details
Main Author: Davis, Jake Daniel
Format: Others
Published: DigitalCommons@CalPoly 2019
Subjects:
CFD
Online Access:https://digitalcommons.calpoly.edu/theses/1968
https://digitalcommons.calpoly.edu/cgi/viewcontent.cgi?article=3359&context=theses
id ndltd-CALPOLY-oai-digitalcommons.calpoly.edu-theses-3359
record_format oai_dc
spelling ndltd-CALPOLY-oai-digitalcommons.calpoly.edu-theses-33592021-08-20T05:02:41Z A Higher-Order Method Implemented in an Unstructured Panel Code to Model Linearized Supersonic Flows Davis, Jake Daniel Since their conception in the 1960s, panel codes have remained a critical tool in the design and development of air vehicles. With continued advancement in computational technologies, today's codes are able to solve flow fields around arbitrary bodies more quickly and with higher fidelity than those that preceded them. Panel codes prove most useful during the conceptual design phase of an air vehicle, allowing engineers to iterate designs, and generate full solutions of the flow field around a vehicle in a matter of seconds to minutes instead of hours to days using traditional CFD methods. There have been relatively few panel codes with the capacity to solve supersonic flow fields, and there has been little recently published work done to improve upon them. This work implements supersonic potential flow methods into Cal Poly’s open source panel code, CPanel. CPanel was originally developed to solve steady, subsonic flows utilizing constant strength source and doublet panels to define the geometry, and an unstructured geometry discretization; it was later extended to include viscous vortex particle wakes and transient modeling. In this thesis, a higher-order method is implemented in CPanel for use in solving linearized supersonic flows, where a higher-order method is one that utilizes at least one singularity element whose order is higher than constant. CPanel results are verified against analytical solutions, such as the Taylor-Maccoll solution for supersonic conical flows and 2D shock-expansion theory, and the PANAIR and MARCAP supersonic panel codes. Results correlate well with the analytical solutions, and show strong agreement with the other codes. 2019-02-01T08:00:00Z text application/pdf https://digitalcommons.calpoly.edu/theses/1968 https://digitalcommons.calpoly.edu/cgi/viewcontent.cgi?article=3359&context=theses Master's Theses DigitalCommons@CalPoly Aerodynamics Supersonic CFD Panel Code CPanel Supersonic Aerodynamics Aerodynamics and Fluid Mechanics
collection NDLTD
format Others
sources NDLTD
topic Aerodynamics
Supersonic
CFD
Panel Code
CPanel
Supersonic Aerodynamics
Aerodynamics and Fluid Mechanics
spellingShingle Aerodynamics
Supersonic
CFD
Panel Code
CPanel
Supersonic Aerodynamics
Aerodynamics and Fluid Mechanics
Davis, Jake Daniel
A Higher-Order Method Implemented in an Unstructured Panel Code to Model Linearized Supersonic Flows
description Since their conception in the 1960s, panel codes have remained a critical tool in the design and development of air vehicles. With continued advancement in computational technologies, today's codes are able to solve flow fields around arbitrary bodies more quickly and with higher fidelity than those that preceded them. Panel codes prove most useful during the conceptual design phase of an air vehicle, allowing engineers to iterate designs, and generate full solutions of the flow field around a vehicle in a matter of seconds to minutes instead of hours to days using traditional CFD methods. There have been relatively few panel codes with the capacity to solve supersonic flow fields, and there has been little recently published work done to improve upon them. This work implements supersonic potential flow methods into Cal Poly’s open source panel code, CPanel. CPanel was originally developed to solve steady, subsonic flows utilizing constant strength source and doublet panels to define the geometry, and an unstructured geometry discretization; it was later extended to include viscous vortex particle wakes and transient modeling. In this thesis, a higher-order method is implemented in CPanel for use in solving linearized supersonic flows, where a higher-order method is one that utilizes at least one singularity element whose order is higher than constant. CPanel results are verified against analytical solutions, such as the Taylor-Maccoll solution for supersonic conical flows and 2D shock-expansion theory, and the PANAIR and MARCAP supersonic panel codes. Results correlate well with the analytical solutions, and show strong agreement with the other codes.
author Davis, Jake Daniel
author_facet Davis, Jake Daniel
author_sort Davis, Jake Daniel
title A Higher-Order Method Implemented in an Unstructured Panel Code to Model Linearized Supersonic Flows
title_short A Higher-Order Method Implemented in an Unstructured Panel Code to Model Linearized Supersonic Flows
title_full A Higher-Order Method Implemented in an Unstructured Panel Code to Model Linearized Supersonic Flows
title_fullStr A Higher-Order Method Implemented in an Unstructured Panel Code to Model Linearized Supersonic Flows
title_full_unstemmed A Higher-Order Method Implemented in an Unstructured Panel Code to Model Linearized Supersonic Flows
title_sort higher-order method implemented in an unstructured panel code to model linearized supersonic flows
publisher DigitalCommons@CalPoly
publishDate 2019
url https://digitalcommons.calpoly.edu/theses/1968
https://digitalcommons.calpoly.edu/cgi/viewcontent.cgi?article=3359&context=theses
work_keys_str_mv AT davisjakedaniel ahigherordermethodimplementedinanunstructuredpanelcodetomodellinearizedsupersonicflows
AT davisjakedaniel higherordermethodimplementedinanunstructuredpanelcodetomodellinearizedsupersonicflows
_version_ 1719460495128264704