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

^*此作品的通讯作者

航空科学与工程学院

Beihang University

科研成果: 期刊稿件 › 文章 › 同行评审

1 引用（Scopus）

摘要

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.

源语言	英语
页（从-至）	395-398
页数	4
期刊	Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics
卷	28
期	4
出版状态	已出版 - 8月 2002

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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.",

keywords = "Aerodynamics, Computation fluid dynamics, Guided missiles",

author = "Huang, \{Xian Lu\} and Chao Yan and Liang Chen and Long, \{Yao Song\}",

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AU - Chen, Liang

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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

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SN - 1001-5965

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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

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