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Wave angle for oblique detonation waves
Authors:S. A. Ashford  G. Emanuel
Affiliation:(1) School of Aerospace and Mechanical Engineering, The University of Oklahoma, 73019-0601 Norman, OK, USA
Abstract:The flow field associated with a steady, planar, oblique detonation wave is discussed. A revision is provided forbeta-theta diagrams, wherebeta is the wave angle andtheta is the ramp angle. A new solution is proposed for weak underdriven detonation waves that does not violate the second law. A Taylor wave, encountered in unsteady detonation waves, is required. Uniqueness and hysteresis effects are also discussed.This article was processed using Springer-Verlag TEX Shock Waves macro package 1.0 and the AMS fonts, developed by the American Mathematical Society.
Keywords:Chapman-Jouguet condition  Oblique detonation wave  Taylor wave  Uniqueness and hysteresis effects
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