NASA NTRS · 19870058001
A mixing augmentation technique for hypervelocity scramjets
Abstract
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.
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Kumar, A., Bushnell, D. M., Hussaini, M. Y.. 1987-06-01. A mixing augmentation technique for hypervelocity scramjets. https://ntrs.nasa.gov/citations/19870058001
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