CRITERIA FOR SELF-IGNITION OF SUPERSONIC HYDROGEN-AIR MIXTURES

摘要

A correlation of available self-ignition data for supersonic hydrogen-air mixtures in configurations representative of scramjet combustors has been made. The correlation was examined in light of simplified ignition-limit models. The data and model included cases of injection from transverse fuel jets on walls, transverse jets behind swept and unswept steps, and transverse injection ahead of swept and unswept steps and strut bases. The results provide useful guidance for predicting self-ignition in a variety of applications. The likely regions for self-ignition in a combustor are given in order of merit.