7、This paper presents a method of characteristics to calculate the structure of the detonation wave in condensed explosive by the decay shock curve data obtained in the aquarium test.
11、The propagation of one dimensional divergent detonation waves is studied in this paper.
15、The present experimental investigation attempts to understand the propagation of gaseous detonation waves in a section lined with perforated steel plate.
3、Using DYNA3D finite element codes, key technical problems such as propagation of detonation wave, case deforming driven by detonation, scattering characteristics of fragment are numerically simulated.
8、It shows that the boundary layer induced behind a 2 ATM 2h2 + O2, mixture detonation wave may undergo a transition from laminar to turbulent and then turn out a turbulent boundary layer.
13、The present experimental investigation attempts to understand the attenuation of detonation waves propagating through an absorbing material lining section.
2、Application of new type ion probe in detonation wave speed measurement
9、Effects of fuel-supply position on detonation waves and working frequency in an aero-valve pulse detonation engine
16、A simple approximate calculation method is given, which can exactly reconstruct the long distance non ideal propagation of detonation waves in the spherical shell of the charge.
6、The detonation wave resistance of multi-layer structures composed of Kevlar composites and amour steels was studied by using simulation test device.
1、The detonation wave ignition technique is suitable to synchronization ignition of multi-chamber liquid rocket engine.
12、As an example, the isobars are plotted for strong detonation waves passing over a wedge surface.
10、A pulse detonation rocket engine (PDRE) is a new propulsion system that generates thrust by using high-temperature and high-pressure air produced by pulse detonation waves.
14、An analytical solution is obtained for the diffraction of strong detonation waves by a stationary two-dimensional thin airfoil.
5、The numerical results agree well with experimental data and provide theoretical basis for engineering design of detonation wave igniter.
4、Experimentalresults show that the steadiness and the repeatability of the flow be-hind detonation wave are excellent.
國文精選館
