Time-resolved size, velocity, and temperature statistics of aluminum combustion in solid rocket propellants-Reference-Cited by-同舟云学术

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Time-resolved size, velocity, and temperature statistics of aluminum combustion in solid rocket propellants

Published:2021 Issue:3 Volume:38 Page:4417-4424
ISSN:1540-7489
Container-title:Proceedings of the Combustion Institute
language:en
Short-container-title:Proceedings of the Combustion Institute

Author:

Marsh Andrew W.^ORCID,Wang Gwendolyn T.^ORCID,Heyborne Jeffery D.,Guildenbecher Daniel R.^ORCID,Mazumdar Yi Chen^ORCID

Funder

U.S. Department of Energy

National Nuclear Security Administration

Laboratory Directed Research and Development

Sandia National Laboratories

Publisher

Elsevier BV

Subject

Physical and Theoretical Chemistry,Mechanical Engineering,General Chemical Engineering

Reference37 articles.

1. Burning Aluminum Particles Inside a Laboratory-Scale Solid Rocket Motor

2. RTO/VKI Special Course on Internal Aerodynamics in Solid Rocket Propulsion;Beckstead,2002

3. Numerical Simulation of Single Aluminum Particle Combustion (Review)

4. TEMPERATURE MEASUREMENTS OF ALUMINUM PARTICLES BURNING IN CARBON DIOXIDE

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