Computation based on the Simons model for vacuum plume

Jian Hua Zhang; Guo Biao Cai

Computation based on the Simons model for vacuum plume

Jian Hua Zhang^*
, Guo Biao Cai

^*Corresponding author for this work

School of Astronautics

Beihang University

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

2 Scopus citations

Abstract

The plume from the attitude controlling rocket motor nozzle has an obvious effect on the aircraft in vacuum. The computation based on the Simons model for vacuum plume was presented, which considers the expansion of the isentropic core and boundary layer. The vacuum plume parameters distribution was obtained. It is shown that the Simons model is a rapid estimation method for vacuum plume calculation in the design of the attitude controlling rocket motor nozzle used on the satellite, airship and other aircraft, as well as its test research.

Original language	English
Pages (from-to)	406-409
Number of pages	4
Journal	Tuijin Jishu/Journal of Propulsion Technology
Volume	23
Issue number	5
State	Published - Oct 2002

Keywords

Attitude controlling rocket engine
High altitude environment
Numerical calculation
Plume

Cite this

@article{d75771bf97634549981d3434b26ddfe6,

title = "Computation based on the Simons model for vacuum plume",

abstract = "The plume from the attitude controlling rocket motor nozzle has an obvious effect on the aircraft in vacuum. The computation based on the Simons model for vacuum plume was presented, which considers the expansion of the isentropic core and boundary layer. The vacuum plume parameters distribution was obtained. It is shown that the Simons model is a rapid estimation method for vacuum plume calculation in the design of the attitude controlling rocket motor nozzle used on the satellite, airship and other aircraft, as well as its test research.",

keywords = "Attitude controlling rocket engine, High altitude environment, Numerical calculation, Plume",

author = "Zhang, \{Jian Hua\} and Cai, \{Guo Biao\}",

year = "2002",

month = oct,

language = "英语",

volume = "23",

pages = "406--409",

journal = "Tuijin Jishu/Journal of Propulsion Technology",

issn = "1001-4055",

publisher = "China Aerospace Science and Industry Corp",

number = "5",

}

TY - JOUR

T1 - Computation based on the Simons model for vacuum plume

AU - Zhang, Jian Hua

AU - Cai, Guo Biao

PY - 2002/10

Y1 - 2002/10

N2 - The plume from the attitude controlling rocket motor nozzle has an obvious effect on the aircraft in vacuum. The computation based on the Simons model for vacuum plume was presented, which considers the expansion of the isentropic core and boundary layer. The vacuum plume parameters distribution was obtained. It is shown that the Simons model is a rapid estimation method for vacuum plume calculation in the design of the attitude controlling rocket motor nozzle used on the satellite, airship and other aircraft, as well as its test research.

AB - The plume from the attitude controlling rocket motor nozzle has an obvious effect on the aircraft in vacuum. The computation based on the Simons model for vacuum plume was presented, which considers the expansion of the isentropic core and boundary layer. The vacuum plume parameters distribution was obtained. It is shown that the Simons model is a rapid estimation method for vacuum plume calculation in the design of the attitude controlling rocket motor nozzle used on the satellite, airship and other aircraft, as well as its test research.

KW - Attitude controlling rocket engine

KW - High altitude environment

KW - Numerical calculation

KW - Plume

UR - https://www.scopus.com/pages/publications/0036820369

M3 - 文章

AN - SCOPUS:0036820369

SN - 1001-4055

VL - 23

SP - 406

EP - 409

JO - Tuijin Jishu/Journal of Propulsion Technology

JF - Tuijin Jishu/Journal of Propulsion Technology

IS - 5

ER -

Computation based on the Simons model for vacuum plume

Abstract

Keywords

Other files and links

Fingerprint

Cite this