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Massachusetts Institute of Technology

A doublet panel method for generalized supersonic lifting surfaces

Abstract

dc:description.abstract

An improved doublet panel method for calculating the aerodynamic properties of lifting surfaces in supersonic flows is derived and implemented. The lifting surfaces are discretized into an arbitrary number of doublet panels with unknown singularity strength, whose perturbation velocity potentials satisfy the supersonic Prandtl-Glauert equation. To prevent field singularities in the potential and velocity, the doublet strength of each panel is piecewise linear and continuous in the streamwise direction. In addition, the panels can be swept at different angles at their leading and trailing edges, allowing for generalized lifting surfaces to be analyzed. The component of the perturbation velocity that is normal to the lifting surface at each specified control point induced by each doublet panel is calculated. Applying the flow tangency boundary condition at the control points forms a linear system that is solved for the difference in doublet strength between the trailing and leading edges of each panel. The perturbation velocity components of this method are compared to those of the Woodward method. The numerical solutions of this method are compared to the analytical solutions of some test cases. Convergence is obtained for both the lift coefficient and the perturbation velocity component distribution.

Degree

thesis:*
Department dc:contributor.department
Massachusetts Institute of Technology. Department of Aeronautics and Astronautics.
Grantor dc:publisher
Massachusetts Institute of Technology
Year dc:date.issued
2017

Author and committee

dc:creator, dc:contributor.*
Author dc:creator
  • Hoskin, Dominique (Dominique Sampson)
Advisor dc:contributor.advisor
  • Mark Drela.

Subjects

dc:subject × 1

Rights

dc:rights
Statement dc:rights
  • MIT theses are protected by copyright. They may be viewed, downloaded, or printed from this source but further reproduction or distribution in any format is prohibited without written permission.
Language dc:language.iso
eng

Identifiers

dc:identifier.*
Handle dc:identifier.uri
http://hdl.handle.net/1721.1/113724
OAI identifier oai:identifier
oai:dspace.mit.edu:1721.1/113724

Chain of custody

source
Harvested from
MIT
Base URL
dspace.mit.edu/oai/request
Last updated
2026-07-22
Source record
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citation

Hoskin, Dominique (Dominique Sampson). A doublet panel method for generalized supersonic lifting surfaces. Massachusetts Institute of Technology, 2017. http://hdl.handle.net/1721.1/113724