GOAD 发表于 2025-3-28 15:20:35
http://reply.papertrans.cn/47/4606/460558/460558_41.png格言 发表于 2025-3-28 19:40:51
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会议 发表于 2025-3-29 00:18:22
http://reply.papertrans.cn/47/4606/460558/460558_43.pngAnthem 发表于 2025-3-29 05:29:56
C. J. Sands,A. M. Milne,L. J. Clifford,G. O. Thomas喃喃诉苦 发表于 2025-3-29 10:17:34
http://reply.papertrans.cn/47/4606/460558/460558_45.pngFabric 发表于 2025-3-29 12:13:21
http://reply.papertrans.cn/47/4606/460558/460558_46.pngConjuction 发表于 2025-3-29 19:38:36
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 发表于 2025-3-29 21:07:39
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 ofBOLT 发表于 2025-3-30 01:01:56
http://reply.papertrans.cn/47/4606/460558/460558_49.pngBone-Scan 发表于 2025-3-30 05:36:45
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.