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International Journal of Energetic Materials and Chemical Propulsion
ESCI SJR: 0.28 SNIP: 0.421 CiteScore™: 0.9

ISSN 印刷: 2150-766X
ISSN オンライン: 2150-7678

International Journal of Energetic Materials and Chemical Propulsion

DOI: 10.1615/IntJEnergeticMaterialsChemProp.v6.i4.20
pages 425-439

A NEW APPROACH TO CHEMICAL MICROPROPULSION − CAN WE USE BOUNDARY LAYERS TO CONTROL COMBUSTION?

Elaine S. Oran
Department of Aerospace Engineering, Texas A&M University, College Station, TX 77832, USA

要約

The presence of boundary layers in combustion chambers can lead to different and unexpected phenomena that alter idealized pictures of reactive flow dynamics. This paper describes two different combustion phenomena in two very different flow regimes: the boundary-accelerated laminar flame, involving only laminar flames and laminar flow, and the detonationless supersonic flame, involving shocks, turbulent flow, and possible detonations. These boundary-induced phenomena can be used to explain observed phenomena, and to promote or control combustion in propulsion and micropropulsion devices.


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