Numeric Simulation for Combustion Instability of Liquid Propellant Rocket Engine

Numeric Simulation for Combustion Instability of Liquid Propellant Rocket Engine

Author(s):

Yuhui, HUANG ( Department of Aerospace Technology National University of Defense Technology )
Jin, ZHOU
Zhenguo, WANG

Publication title:

AIAA paper

Title of ser.:

AIAA Paper : AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Ser. no.:

2000

Pub. date:

2000

Serial:

2000-3297

Paper no.:

00-3297

Page(from):

1

Page(to):

8

Pub. info.:

American Institute of Aeronautics and Astronautics

ISSN:

01463705

Language:

English

Call no.:

A07400

Type:

Technical Paper

Details

TDL ID:	ZA00050879
Series ID:	PA00000151
Conf. info. (Name):	AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Conf. info. (Number):	36th
Conf. info. (Venue):	Huntsville, AL
Conf. info. (Date):	2000.07.16-2000.07.19
Note for article:	36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference 17-19 July, 2000 Huntsville, Alabama

Similar Items:

1 Technical Paper Nonlinear Thermodynamic Analyses of Combustion Instability in Rocket Engine Yuhui, HUANG, Zhenguo, WANG, Jin, ZHOU American Institute of Aeronautics and Astronautics	7 Technical Paper Global Model of Liquid Rocket Engine Combustion Instability Based on Chemistry Dynamics. Yuhui, H., Wentao, Z., Zhenguo, W., Jin, Z. American Institute of Aeronautics and Astronautics
2 Technical Paper A Nonlinear Analytical Model of High-Frequency Combustion Instability in Rocket Engine Zhenguo, WANG, Yuhui, HUANG, Jin, ZHOU American Institute of Aeronautics and Astronautics	8 Technical Paper Flowrate and acoustics characteristics of coaxial swirling injector of hydrogen/oxygen rocket engine Zhou, Jin, Hu, Xiaoping, Huang, Yuhui, Wang, Zhenguo American Institute of Aeronautics and Astronautics
3 Technical Paper Numerical analysis model for radial combustion instability in liquid propellant engine Weidong, Liu, Zhenguo, Wang, Jin, Zhou, Fengchen, Zhuang American Institute of Aeronautics and Astronautics	9 Technical Paper The Numerical Simulation of The Hot flow Field In Tripropellant LRE Qinglian,Li, Yuhui,Huang, Zhenguo,Wang American Institute of Aeronautics and Astronautics
4 Technical Paper Numerical simulation of unsteady flow in liquid propellant rocket engine with PISO algorithm Weidong, Liu, Zhenguo, Wang, Jin, Zhou, Fengchen, Zhuang American Institute of Aeronautics and Astronautics	10 Technical Paper Acoustic model for the self-oscillation of coaxial swirl injector Yuhui, Huang, Jin, Zhou, Xiaoping, Hu, Zhenguo, Wang American Institute of Aeronautics and Astronautics
5 Technical Paper The Characteristics of Acoustic Waves and Acoustic Cavities to Combustion Instability Jin, Zhou, Yuhui, Huang, Zhenguo, Wang American Institute of Aeronautics and Astronautics	11 Technical Paper The Optimization of Boundary Layer Trip in Advanced Chambers Zhenguo, Wang, Yuhui, Huang, Jin, Zhou, Zhongguang, Zhang American Institute of Aeronautics and Astronautics
6 Technical Paper The characteristics of acoustic waves and acoustic cavities to combustion instability Jin, Zhou, Yuhui, Huang, Zhenguo, Wang American Institute of Aeronautics and Astronautics	12 Technical Paper The optimization of boundary layer trip in advanced chambers Zhenguo, Wang, Yuhui, Huang, Jin, Zhou, Zhongguang, Zhang American Institute of Aeronautics and Astronautics

1

2

3

4

5

6

7

8

9

10

11

12