Igniton of 2H2-O2 Mixtures by Means of Shock Waves |
Common terms and phrases
acla adiabatic compression ignition AMBIENT INITIAL TEMPS annular clearance ax/a B.S. degree BASED UPON SIMPLE BUFFER compression ignition temperature condition CORNELL UNIVERSITY LIBRARY CORRECTED FOR ANNULUS DATA FOR AMBIENT Data from Fig DATA OF FIG DETONATION DATA DETONATION No DETONATION drum camera record elevated initial temperatures END FLANGE flow at section gas bottle gas mixtures initially IMEG incident shock INITIAL TEMPS BASED initially at room inner wall INTERFACE ISENTROPIC J. A. Fay LARGE TUBE Limit of Ignition LUCITE END PLATE Mach number nition occur oscilloscope Pc/P₁ PREAMP premixed PRESSURE PICK-UP Ratio of specific reflected shock REFLECTION OLD END REGION OF STEADY results are plotted series of tests shock of strength shock strength shock tube shock velocity shock wave SIMPLE REFLECTION OLD SLIDING DIAPHRAGM SLIDING PLATE SOLENOID space-time diagram specific heats STRAIN GAGE strength M(W sweep Thesis THYRATRON CIRCUIT TRIGGER tube wall uniform shock uniform temperature window sections