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Experimental Apparatus and Procedure
Recommendations for Further Improvements
1 other sections not shown
20 nanosecond 35mm film record Acoustic Reflector adjustable amplification beam splitters Beasley Boost Logic V+ Close-up View conical section constant Cornell University CP ref curvature Determine Shock Wave diaphragm disconnect flange driver gas driver pressures necessitated driver section Equation experimental apparatus feet ferograms Figure 15 Figure 17 Figure 19b focused shock wave focused wave fringe pattern fringe shift fuzziness helium-neon laser hence incoming wave Infinite Fringe Interferogram interferogram of focused laboratory Mach number Mach-Zehnder interferometer Moire Pattern N-waves NASA necessary no-flow interferogram Nonlinear Acoustic oscilloscope Oscilloscope Traces Output Overpressures at Caustic preamplifier pressure amplitudes measured pressure signatures produced pulsed ruby laser quantitative raising the Mach range ray caustic rotating mirror camera Schematic of Microphone Seebass shock tube shown in Figure signal Sonic Boom sound speed gradient special ultra-high-speed steel rods superboom test runs test section thick Trigger Light Source trigger the laser Typical 35mm Film Version of Caustic weak shock waves