combustion bomb
1.Numerical Simulation for Flame Kernel Initiation and Early Development in a Constant Volume Combustion Bomb
2.The multifunction combustion bomb system was composed of the bomb body,mixture allocate system,air/fuel blend system,injection system,spark ignition system,control system and combustion data capture and analysis system etc.
4.Methods The combustion rate of propellants of different PNP/PVB, RDX/binder ratio have been tested by the manometric bomb test.
5.The effects of the content of Hexogen(RDX)and Nitroguanidine(NGu) on the combustion behavior of nitramine propellants under low pressure were studied in the closed bomb. The combustion data of six kind of nitramine propellants with different ratio of RDX /NGu were obtained from 20 MPa to 60 MPa by the closed bomb test.
6.Determination of Sulfur in Diesel Oil Certified Reference Materials by Oxygen-bomb-combustion ICP-OES
7.The chief characteristic that determines the quantity- of energy recoverable from the combustion of mixed waste paper (MWP) is the thermal energy of the material as measured by a bomb calorimeter.
8.On the special combustion performance of the high energy nitramine propellants which were higher pressure exponent for burning rate in bomb, this paper studies and analyzes the basic combustion characteristics upon the gun bore for the propellants by using the 30mm high pressure simulated gun tests and comparing to the single base propellant.
9.The combustion parameters such as co-volume and impetus of the studied explosives were obtained through two methods, one is the standard Closed Bomb Test (CBT) and the other is theoretic calculating with VLWR EOS. The calculated values agreed well with experimental data.
10.The desertation introduces the design procedure and configuration of the bomb, which includes the mixture gas preparation, heating, ignition, combustion pressure measurement systems, CCD camera and data aquisition system.
