1982 …2018

Research output per year

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Research Output

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Paper

A simplified model for composite propellant burning rate

Knott, G. M., Brewster, M. Q. & Jackson, T. L., Jan 1 1999.

Research output: Contribution to conferencePaper

A two-dimensional model of composite propellant flame structure and burning rate

Knott, G. M. & Brewster, M. Q., Jan 1 2000.

Research output: Contribution to conferencePaper

Combustion modeling of composite solid propellants with finite peclet number

Knott, G. M. & Brewster, M. Q., Jan 1 1998.

Research output: Contribution to conferencePaper

Computational simulation of nonlinear L* Combustion instability in solid rockets

Tang, K. C. & Brewster, M. Q., Jan 1 1999.

Research output: Contribution to conferencePaper

Dynamic combustion of AP composite propellents: Ignition pressure spike

Tang, K. C. & Brewster, M. Q., Dec 1 2001.

Research output: Contribution to conferencePaper

Flame structure of ap/binder sandwiches from emission imaging

Chorpening, B. T. & Brewster, M. Q., Jan 1 1999.

Research output: Contribution to conferencePaper

Flame structure of wide distribution AP/HTPB composite solid propellants from emission imaging

Chorpening, B. T. & Brewster, M. Q., Jan 1 1998.

Research output: Contribution to conferencePaper

Ignition dynamics of high explosives

Ali, A. N., Son, S. F., Sander, R. K., Asay, B. W. & Brewster, M. Q., Jan 1 1999.

Research output: Contribution to conferencePaper

In-situ measurements of alumina particle size and optical constants in composite solid propellant flames

Brewster, Q. & Parry, D. L., Jan 1 1987.

Research output: Contribution to conferencePaper

Laser-recoil response of AP-HTPB propellants (1-5 atm): Selective pyrolysis response

Hickman, S. R. & Brewster, M. Q., Jan 1 1999.

Research output: Contribution to conferencePaper

Modeling combustion of laminate propellants with fine ammonium perchlorate

Genevieve, P. & Brewster, M. Q., Dec 1 2002.

Research output: Contribution to conferencePaper

Multi-scale modeling of solid rocket motors: Time integration methods from computational aerodynamics applied to stable quasi-steady motor burning

Stewart, D. S., Tang, K. C., Yoo, S., Brewster, M. Q. & Kuznetsov, I. R., Dec 1 2005, p. 6789-6798. 10 p.

Research output: Contribution to conferencePaper

Nonlinear dynamic combustion in solid rockets: L*-effects

Tang, K. C. & Brewster, M. Q., Dec 1 2000.

Research output: Contribution to conferencePaper

Nonlinear dynamic combustion in solid rockets: L*-effects

Tang, K. C. & Brewster, M. Q., Jan 1 2000.

Research output: Contribution to conferencePaper

Solid propellant grain design and burnback simulation using a minimum distance function

Willcox, M. A., Brewster, M. Q., Tang, K. C. & Stewart, D. S., Dec 1 2005.

Research output: Contribution to conferencePaper

Steady deflagration of hmx with simple kinetics: A new modeling paradigm

Ward, M. J., Son, S. F. & Brewster, M. Q., Jan 1 1997.

Research output: Contribution to conferencePaper

Temperature measurement of a burning surface by a thermocouple II

Ishihara, A., Tang, K. C. & Brewster, M. Q., Dec 1 2005.

Research output: Contribution to conferencePaper

Thermal analysis of gas assisted low power laser drilling of metals

Patel, R. S. & Brewster, M. Q., Jan 1 1989.

Research output: Contribution to conferencePaper

Unsteady combustion of solid propellants: Simplified kinetics modeling

Brewster, M. Q., Jan 1 2000.

Research output: Contribution to conferencePaper

Unsteady pressure combustion response of AP composite propellants

Saarloos, B. & Brewster, M. Q., Dec 1 2002.

Research output: Contribution to conferencePaper