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.
A mixing augmentation technique for hypervelocity scramjets
01.06.1987
Aufsatz (Konferenz)
Keine Angabe
Englisch