1968 …2018
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Research Output 1968 2018

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Conference contribution
2013

Heat transfer effects in nano-aluminum combustion

Allen, D., Krier, H. & Glumac, N. G., 2013, 8th US National Combustion Meeting 2013. Western States Section/Combustion Institute, Vol. 2. p. 957-969 13 p.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Aluminum
heat transfer
accommodation coefficient
Heat transfer
aluminum
2010

Optical spectroscopy of fireballs from metallized reactive materials

Glumac, N. G., Krier, H., Lynch, P. & Peuker, J. M., Dec 13 2010, 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. 2010-0695. (48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Emission spectroscopy
Dye lasers
Fiber optics
Wavelength
Temperature
2009

Size distribution effects in heterogeneous shock tube burntime experiments

Lynch, P., Krier, H. & Glumac, N. G., 2009, 45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Shock tubes
shock tubes
Water vapor
water vapor
experiment

The emissivity of micro- and nano- particles in non-reacting environments

Lynch, P., Krier, H. & Glumac, N. G., 2009, 47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. 2009-0640

Research output: Chapter in Book/Report/Conference proceedingConference contribution

emissivity
aluminum oxide
aluminum oxides
Alumina
wavelength

The presence of gas phase species in micro- and nano-aluminum combustion

Lynch, P., Fiore, G., Krier, H. & Glumac, N. G., Dec 1 2009, 47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. 2009-0638. (47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

aluminum
combustion
vapor phases
Aluminum
Vapors
2008

Combustion of Aluminum particles in the transition regime between the diffusion and kinetic limits

Lynch, P., Glumac, N. & Krier, H., Dec 1 2008, 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. (44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

aluminum
combustion
Aluminum
kinetics
Kinetics
2007

Combustion of 5-μim aluminum particles in high temperature, high pressure, water vapor environments

Lynch, P., Glumac, N. & Krier, H., Dec 10 2007, Collection of Technical Papers - 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference. p. 6264-6270 7 p. (Collection of Technical Papers - 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference; vol. 6).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

water vapor
aluminum
combustion
oxidizers
particle
2006

Modeling the combustion of nano-sized aluminum particles

Aita, K., Glumac, N., Vanka, S. P. & Krier, H., Dec 1 2006, Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting. p. 14026-14045 20 p. (Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting; vol. 19).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

aluminum
combustion
Aluminum
oxygen
Oxygen

Shock tube measurements of combustion of nano-aluminum

Bazyn, T., Krier, H. & Glumac, N. G., Dec 1 2006, Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting. p. 14046-14053 8 p. (Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting; vol. 19).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Shock tubes
shock tubes
aluminum
combustion
Aluminum
2005

The combustion characteristics of 10-micron aluminum particles at elevated temperature and pressure

Bazyn, T., Glumac, N. G. & Krier, H., 2005, 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Aluminum
Particle size
Solid propellants
Oxygen
Emission spectroscopy
2002

Ultrasonic measurement of the pressure-coupled response function at low frequency for composite solid propellants

Hafenrichter, T. J., Murphy, J. J. & Krier, H., Dec 1 2002, 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. (38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Ultrasonic measurement
Solid propellants
Propellants
Composite materials
Fuel burners
2000

Combustion of aluminum in solid rocket motor flows

Melcher, J. C., Brzozowski, J. T., Krier, H. & Burton, R. L., 2000, 35th Intersociety Energy Conversion Engineering Conference and Exhibit.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Rocket engines
Aluminum
Smoke
Ignition
Flow fields

Numerical analysis of the stability of solid rocket motors: Two-phase flow aspects

Daniel, E., Lee, M. G., Murphy, J. J. & Krier, H., 2000, 38th Aerospace Sciences Meeting and Exhibit.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Rocket engines
Convergence of numerical methods
two phase flow
rockets
Two phase flow

Response function measurement using an ultrasonic technique in an oscillatory burner

Murph, J. J., Chai, S., Brdar, C. R. & Krier, H., 2000, 35th Intersociety Energy Conversion Engineering Conference and Exhibit.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Propellants
Fuel burners
Ultrasonics
Nozzles
Solid propellants
1998

Precision techniques for measuring burning rates of solid propellants during pressure transients

Murphy, J. J., Martin, A. O. & Krier, H., 1998, 36th AIAA Aerospace Sciences Meeting and Exhibit. American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA 98-0560

Research output: Chapter in Book/Report/Conference proceedingConference contribution

transient pressures
solid propellants
burning rate
Solid propellants
Propellants

Ultrasound measurements of solid propellant burning rates: Theory and application

Murphy, J. J. & Krier, H., 1998, 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. American Institute of Aeronautics and Astronautics Inc, AIAA

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Solid propellants
Ultrasonics
Propellants
Pressure effects
Surface structure
1995

Application of internal Langmuir diagnostics to arcjets

Tiliakos, N. T., Burton, R. L. & Krier, H., Jan 1 1995, 31st Joint Propulsion Conference and Exhibit. American Institute of Aeronautics and Astronautics Inc, AIAA, p. 1-15 15 p. (31st Joint Propulsion Conference and Exhibit).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Nozzles
Anodes
Electric potential
Langmuir probes
Joule heating
1991

Effect of radiative heat feedback on burning rate of metalized propellants

Ishihara, A., Brewster, M. Q., Sheridan, T. A. & Krier, H., 1991, ASME/JSME Thermal Engineering Joint Conference. Publ by ASME, p. 35-40 6 p.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Propellants
Feedback
Thermocouples
Magnesium
Boron
1984

ANALYSIS OF DEFLAGRATION TO SHOCK TO DETONATION TRANSITION (DSDT) IN POROUS ENERGETIC SOLID PROPELLANTS.

Butler, P. B. & Krier, H., Dec 1 1984, AGARD Conference Proceedings. 367 ed. AGARD, p. 5. 1-5. 10 (AGARD Conference Proceedings; no. 367).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Solid propellants
Detonation
Propellants