Computation of internal flow with free surfaces using artificial compressibility

Dartzi Pan; Yi Sheng Yang; Chih Hao Chang

doi:10.1080/10407799808915026

Computation of internal flow with free surfaces using artificial compressibility

Dartzi Pan
, Yi Sheng Yang
, Chih Hao Chang

Department of Aeronautics and Astronautics

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

5 Citations (Scopus)

Abstract

In this article an upwind flux-differencing scheme using artificial compressibility is generalized to allow time-accurate computation of incompressible flows on a dynamic grid system. By treating the free surface as a moving grid line that connects in a Lagrangian fashion, the scheme can be applied to solve a variety of free surface flows of moderate surface deformation. The surface tension effects can also be included using a source term and via boundary condition.

Original language	English
Pages (from-to)	119-134
Number of pages	16
Journal	Numerical Heat Transfer, Part B: Fundamentals
Volume	33
Issue number	1
DOIs	https://doi.org/10.1080/10407799808915026
Publication status	Published - 1998

All Science Journal Classification (ASJC) codes

Numerical Analysis
Modelling and Simulation
Condensed Matter Physics
Mechanics of Materials
Computer Science Applications

Access to Document

10.1080/10407799808915026

Cite this

@article{5956e531fb2d41b1a626708a653a31a9,

title = "Computation of internal flow with free surfaces using artificial compressibility",

abstract = "In this article an upwind flux-differencing scheme using artificial compressibility is generalized to allow time-accurate computation of incompressible flows on a dynamic grid system. By treating the free surface as a moving grid line that connects in a Lagrangian fashion, the scheme can be applied to solve a variety of free surface flows of moderate surface deformation. The surface tension effects can also be included using a source term and via boundary condition.",

author = "Dartzi Pan and Yang, \{Yi Sheng\} and Chang, \{Chih Hao\}",

note = "Funding Information: Received 20 August 1996; accepted 4 August 1997. This work is partially supported by the National Science Council, Republic of China, under contract NSC86-2212-EOO6-058. Address correspondence to Prof. Dartzi Pan, Institute of Aeronautics and Astronautics, National Cheng Kung University, Tainan, Taiwan 70101, ROC. E-mail: [email protected]",

year = "1998",

doi = "10.1080/10407799808915026",

language = "English",

volume = "33",

pages = "119--134",

journal = "Numerical Heat Transfer, Part B: Fundamentals",

issn = "1040-7790",

publisher = "Taylor and Francis Ltd.",

number = "1",

}

TY - JOUR

T1 - Computation of internal flow with free surfaces using artificial compressibility

AU - Pan, Dartzi

AU - Yang, Yi Sheng

AU - Chang, Chih Hao

N1 - Funding Information: Received 20 August 1996; accepted 4 August 1997. This work is partially supported by the National Science Council, Republic of China, under contract NSC86-2212-EOO6-058. Address correspondence to Prof. Dartzi Pan, Institute of Aeronautics and Astronautics, National Cheng Kung University, Tainan, Taiwan 70101, ROC. E-mail: [email protected]

PY - 1998

Y1 - 1998

N2 - In this article an upwind flux-differencing scheme using artificial compressibility is generalized to allow time-accurate computation of incompressible flows on a dynamic grid system. By treating the free surface as a moving grid line that connects in a Lagrangian fashion, the scheme can be applied to solve a variety of free surface flows of moderate surface deformation. The surface tension effects can also be included using a source term and via boundary condition.

AB - In this article an upwind flux-differencing scheme using artificial compressibility is generalized to allow time-accurate computation of incompressible flows on a dynamic grid system. By treating the free surface as a moving grid line that connects in a Lagrangian fashion, the scheme can be applied to solve a variety of free surface flows of moderate surface deformation. The surface tension effects can also be included using a source term and via boundary condition.

UR - https://www.scopus.com/pages/publications/0031621884

UR - https://www.scopus.com/pages/publications/0031621884#tab=citedBy

U2 - 10.1080/10407799808915026

DO - 10.1080/10407799808915026

M3 - Article

AN - SCOPUS:0031621884

SN - 1040-7790

VL - 33

SP - 119

EP - 134

JO - Numerical Heat Transfer, Part B: Fundamentals

JF - Numerical Heat Transfer, Part B: Fundamentals

IS - 1

ER -

Computation of internal flow with free surfaces using artificial compressibility

Abstract

All Science Journal Classification (ASJC) codes

Access to Document

Other files and links

Fingerprint

Cite this