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 for- diagrams, where is the wave angle and 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 |
本文献已被 SpringerLink 等数据库收录! |
|