A higher order panel method applied to vortex sheet roll-up

H.W.M. Hoeijmakers; W. Vaatstra

doi:10.2514/3.8108

A higher order panel method applied to vortex sheet roll-up

H.W.M. Hoeijmakers, W. Vaatstra

Research output: Contribution to journal › Article › Academic › peer-review

33 Citations (Scopus)

Abstract

The paper describes a computational method for two-dimensional vortex sheet motion in incompressible flow. The procedure utilizes a second-order panel method, an adaptive panel scheme, and a concept for treating highly rolled-up portions of the vortex sheet. Results are presented for the roll-up of the wake behind an elliptically loaded wing, a ring wing (nacelle), a fuselage/part-span flap/wing combination, and a delta wing with leadingedge vortex sheets. The examples demonstrate that the method is capable of describing complicated vortex sheet motion in a reliable and stable manner.

Original language	English
Pages (from-to)	516-523
Number of pages	8
Journal	AIAA journal
Volume	21
Issue number	4
DOIs	https://doi.org/10.2514/3.8108
Publication status	Published - 1 Jan 1983
Externally published	Yes

Access to Document

10.2514/3.8108

Cite this

@article{d63e2480e0fe4d479cad420e5aaaa0fa,

title = "A higher order panel method applied to vortex sheet roll-up",

abstract = "The paper describes a computational method for two-dimensional vortex sheet motion in incompressible flow. The procedure utilizes a second-order panel method, an adaptive panel scheme, and a concept for treating highly rolled-up portions of the vortex sheet. Results are presented for the roll-up of the wake behind an elliptically loaded wing, a ring wing (nacelle), a fuselage/part-span flap/wing combination, and a delta wing with leadingedge vortex sheets. The examples demonstrate that the method is capable of describing complicated vortex sheet motion in a reliable and stable manner.",

author = "H.W.M. Hoeijmakers and W. Vaatstra",

year = "1983",

month = jan,

day = "1",

doi = "10.2514/3.8108",

language = "English",

volume = "21",

pages = "516--523",

journal = "AIAA journal",

issn = "0001-1452",

publisher = "American Institute of Aeronautics and Astronautics Inc. (AIAA)",

number = "4",

}

TY - JOUR

T1 - A higher order panel method applied to vortex sheet roll-up

AU - Hoeijmakers, H.W.M.

AU - Vaatstra, W.

PY - 1983/1/1

Y1 - 1983/1/1

N2 - The paper describes a computational method for two-dimensional vortex sheet motion in incompressible flow. The procedure utilizes a second-order panel method, an adaptive panel scheme, and a concept for treating highly rolled-up portions of the vortex sheet. Results are presented for the roll-up of the wake behind an elliptically loaded wing, a ring wing (nacelle), a fuselage/part-span flap/wing combination, and a delta wing with leadingedge vortex sheets. The examples demonstrate that the method is capable of describing complicated vortex sheet motion in a reliable and stable manner.

AB - The paper describes a computational method for two-dimensional vortex sheet motion in incompressible flow. The procedure utilizes a second-order panel method, an adaptive panel scheme, and a concept for treating highly rolled-up portions of the vortex sheet. Results are presented for the roll-up of the wake behind an elliptically loaded wing, a ring wing (nacelle), a fuselage/part-span flap/wing combination, and a delta wing with leadingedge vortex sheets. The examples demonstrate that the method is capable of describing complicated vortex sheet motion in a reliable and stable manner.

UR - http://www.scopus.com/inward/record.url?scp=0020738315&partnerID=8YFLogxK

U2 - 10.2514/3.8108

DO - 10.2514/3.8108

M3 - Article

AN - SCOPUS:0020738315

SN - 0001-1452

VL - 21

SP - 516

EP - 523

JO - AIAA journal

JF - AIAA journal

IS - 4

ER -

A higher order panel method applied to vortex sheet roll-up

Abstract

Access to Document

Other files and links

Fingerprint

Cite this