Effects of nozzle contour in convergent section and throat on mass flow rate

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

9 Scopus citations

Original language	English
Pages (from-to)	10
Number of pages	1
Journal	Guti Huojian Jishu/Journal of Solid Rocket Technology
Volume	25
Issue number	1
State	Published - Mar 2002

Cite this

@article{bcd2c468bade4d2390937f4f5daa1c2e,

title = "Effects of nozzle contour in convergent section and throat on mass flow rate",

author = "Chen, \{Lin Quan\} and Li, \{Yan Fang\} and Xiao Hou and Dong, \{Xin Gang\}",

year = "2002",

month = mar,

language = "英语",

volume = "25",

pages = "10",

journal = "Guti Huojian Jishu/Journal of Solid Rocket Technology",

issn = "1006-2793",

publisher = "Journal of Solid Rocket Technology",

number = "1",

}

TY - JOUR

T1 - Effects of nozzle contour in convergent section and throat on mass flow rate

AU - Chen, Lin Quan

AU - Li, Yan Fang

AU - Hou, Xiao

AU - Dong, Xin Gang

PY - 2002/3

Y1 - 2002/3

UR - https://www.scopus.com/pages/publications/0036520584

M3 - 文章

AN - SCOPUS:0036520584

SN - 1006-2793

VL - 25

SP - 10

JO - Guti Huojian Jishu/Journal of Solid Rocket Technology

JF - Guti Huojian Jishu/Journal of Solid Rocket Technology

IS - 1

ER -