Nonlinear Dynamic Combustion in Solid Rockets: L*-Effects

Nonlinear Dynamic Combustion in Solid Rockets: L*-Effects

Author(s):

Tang, K. C. ( University of Illinois at Urbana-Champaign )
Brewster, M. Q.

Publication title:

AIAA paper

Title of ser.:

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

Ser. no.:

2000

Pub. Year:

2000

No.:

2000-3572

Paper no.:

00-3572

Page(from):

1

Page(to):

16

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 and Exhibit 16-19 July 2000 / Huntsville, Alabama

Similar Items:

1 Technical Paper Computational Simulation of Nonlinear L Combustion Instability in Solid Rockets* Tang, K. C., Brewster, M.Q. American Institute of Aeronautics and Astronautics	7 Technical Paper High pressure combustion of cryogenic solid fuels for hybrid rockets Larson, C.W., Pfeil, K.L., DeRose, M.E., Carrick, P.G. American Institute of Aeronautics and Astronautics
2 Technical Paper Computational simulation of nonlinear L combustion instability in solid rockets* Tang, K.C., Brewster, M.Q. American Institute of Aeronautics and Astronautics	8 Technical Paper Unsteady Solid Propellant Pressure Combustion Response Using a Piston Burner. Saarloos, B., Brewster, M.Q. American Institute of Aeronautics and Astronautics
3 Technical Paper Dynamic Combustion of AP Composite Propellants: Ignition Pressure Spike Tang,K.C., Brewster,M.Q. American Institute of Aeronautics and Astronautics	9 Technical Paper Combustion modeling of composite solid propellants with finite peclet number Knott, G.M., Brewster, M.Q. American Institute of Aeronautics and Astronautics
4 Technical Paper Modeling Combustion of Hydrazinium Nitroformate. Tang, K.C., Brewster, M.Q. American Institute of Aeronautics and Astronautics	10 Technical Paper Solid Propellant Grain Design and Burnback Simulation using a Minimum Distance Function Willcox, M., Brewster, M., Tang, K., Stewart, D. American Institute of Aeronautics and Astronautics
5 Technical Paper Ignition of Composite Solid Propellants: Model Development, Experiments, and Validation Weber, J.W., Tang, K.C., Brewster, M.Q. American Institute of Aeronautics and Astronautics	11 Technical Paper New paradigm for simplified combustion modeling of energetic solids: branched chain gas reaction Brewster, M.Q., Ward, M.J., Son, S.F. American Institute of Aeronautics and Astronautics
6 Technical Paper Multi-Scale Modeling of Solid Rocket Motors: Time Integration Methods from Computational Aerodynamics Applied to Stable Quasi-Steady Motor Burning Stewart, D., Tang, K., Yoo, S., Brewster, Q., Kuznetsov, I. American Institute of Aeronautics and Astronautics	12 Technical Paper Temperature Measurement of a Burning Surface by a Thermocouple II Ishihara, A., Tang, K., Brewster, M. American Institute of Aeronautics and Astronautics

1

2

3

4

5

6

7

8

9

10

11

12