Titlebook: IUTAM Symposium on Combustion in Supersonic Flows; Proceedings of the I M. Champion,B. Deshaies Conference proceedings 1997 Springer Scienc

GOAD

格言

A. V. Fedorov,V. M. Fominaccharides i.e. alginates, cellulose, chitosan, dextrins, modified starch, proteins and lipids have been studied as nano-carriers. Various othr materials such as, nanoliposomes, niosomes, bilosomes, solid lipid nanoparticles (SLNs), nano-structured lipid carriers (NLCs) and nano-hydrogels have also

會議

Anthem

C. J. Sands,A. M. Milne,L. J. Clifford,G. O. Thomas

喃喃訴苦

Fabric

Conjuction

Flame-Holding Behind a Wedge by Incident Shock Waveson flow was established and the wake region behind the strut was expanded by incident shock waves. Numerical simulation by a two-dimensional compressible flow code with one-step irreversible reaction model was also conducted to investigate the structure of the wake flow and the ignition process and

衰老

Effects of Laminar Flamelet Structures on Supersonic Turbulent Combustionextinction, possibly leading to ignition delay in high speed flow. In the case of hydrogen-air flames, the Lewis number departs from unity due to the high diffusivity of hydrogen, and the effect of non-unity Lewis number may contribute to the energy redistribution, due to the molecular diffusion of

BOLT

Bone-Scan

Shock Tube Investigations of H2 Combustion in a High Temperature Supersonic Air Flow. (Scramjet)onally from the top of small cylindrical tubes immersed into the flow under 30 degree angle, a rather effective mixing could be obtained leading to about 70 % combustion efficiency 30 cm (5 times the height of the duct) downstream of the injection location.