Numerical analysis of complex flow fields around multi-wing missiles and its aerodynamic force computations

Xian Lu Huang; Chao Yan; Liang Chen; Yao Song Long

Numerical analysis of complex flow fields around multi-wing missiles and its aerodynamic force computations

Xian Lu Huang^*
, Chao Yan
, Liang Chen
, Yao Song Long

^*Corresponding author for this work

School of Aeronautic Science and Engineering

Beihang University

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

1 Scopus citations

Abstract

The applications of modified Jameson's scheme to the complex flow around the missiles with canards and tails, have good agreement between computations and experiment data of the standard missile model of U.S.A.. In computations, the latest modifications of Jameson's scheme are adopted to extend applications of the scheme to high supersonic and high Reynolds number flows. The multi-zone technique and 3-D elliptic grid generation method are also employed to precisely simulate the flows.

Original language	English
Pages (from-to)	395-398
Number of pages	4
Journal	Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics
Volume	28
Issue number	4
State	Published - Aug 2002

Keywords

Aerodynamics
Computation fluid dynamics
Guided missiles

Cite this

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title = "Numerical analysis of complex flow fields around multi-wing missiles and its aerodynamic force computations",

abstract = "The applications of modified Jameson's scheme to the complex flow around the missiles with canards and tails, have good agreement between computations and experiment data of the standard missile model of U.S.A.. In computations, the latest modifications of Jameson's scheme are adopted to extend applications of the scheme to high supersonic and high Reynolds number flows. The multi-zone technique and 3-D elliptic grid generation method are also employed to precisely simulate the flows.",

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AU - Long, Yao Song

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Y1 - 2002/8

N2 - The applications of modified Jameson's scheme to the complex flow around the missiles with canards and tails, have good agreement between computations and experiment data of the standard missile model of U.S.A.. In computations, the latest modifications of Jameson's scheme are adopted to extend applications of the scheme to high supersonic and high Reynolds number flows. The multi-zone technique and 3-D elliptic grid generation method are also employed to precisely simulate the flows.

AB - The applications of modified Jameson's scheme to the complex flow around the missiles with canards and tails, have good agreement between computations and experiment data of the standard missile model of U.S.A.. In computations, the latest modifications of Jameson's scheme are adopted to extend applications of the scheme to high supersonic and high Reynolds number flows. The multi-zone technique and 3-D elliptic grid generation method are also employed to precisely simulate the flows.

KW - Aerodynamics

KW - Computation fluid dynamics

KW - Guided missiles

UR - https://www.scopus.com/pages/publications/0036695977

M3 - 文章

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SN - 1001-5965

VL - 28

SP - 395

EP - 398

JO - Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics

JF - Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics

IS - 4

ER -

Numerical analysis of complex flow fields around multi-wing missiles and its aerodynamic force computations

Abstract

Keywords

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