Publication Date:
2019-06-28
Description:
The paper discusses mixing problems in hypervelocity scramjet combustors. Techniques for providing turbulence and/or mixing enhancement are described. One such technique, the oscillating shock interaction, is studied numerically and options for producing oscillatory shock waves for mixing augmentation in scramjet combustors are discussed.
Keywords:
AIRCRAFT PROPULSION AND POWER
Type:
AIAA PAPER 87-1882
Format:
text
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