標(biāo)題: Titlebook: Detonation Control for Propulsion; Pulse Detonation and Jiun-Ming Li,Chiang Juay Teo,Cheng Wang Book 2018 Springer International Publishing [打印本頁] 作者: 娛樂某人 時間: 2025-3-21 19:22
書目名稱Detonation Control for Propulsion影響因子(影響力)
書目名稱Detonation Control for Propulsion影響因子(影響力)學(xué)科排名
書目名稱Detonation Control for Propulsion網(wǎng)絡(luò)公開度
書目名稱Detonation Control for Propulsion網(wǎng)絡(luò)公開度學(xué)科排名
書目名稱Detonation Control for Propulsion被引頻次
書目名稱Detonation Control for Propulsion被引頻次學(xué)科排名
書目名稱Detonation Control for Propulsion年度引用
書目名稱Detonation Control for Propulsion年度引用學(xué)科排名
書目名稱Detonation Control for Propulsion讀者反饋
書目名稱Detonation Control for Propulsion讀者反饋學(xué)科排名
作者: 過濾 時間: 2025-3-21 20:57
Development of Gasturbine with Detonation Chamber, achieved are presented. It was found that for conditions when the GTD-350 engine was supplied by gaseous hydrogen or by dual-fuel, Jet-A and gaseous hydrogen, thermal efficiency of the engine could be improved even by 5–7% as compared to the efficiency of the base engine.作者: Between 時間: 2025-3-22 04:25
Flow Structure in Rotating Detonation Engine with Separate Supply of Fuel and Oxidizer: Experiment specific impulse. With the growth of the specific mass flow rate of reactive mixture, the operation process, on the one hand, becomes more stable, and on the other hand, the number of detonation waves simultaneously rotating in one direction in the combustor annulus increases. The results of DLRE fi作者: badinage 時間: 2025-3-22 08:19 作者: 你不公正 時間: 2025-3-22 11:26
On the Investigation of Detonation Re-initiation Mechanisms and the Influences of the Geometry Confmes, which is discovered to be the main reason leading to the discrepancies between the previous similar studies. The width of the bifurcation channel is also critical as it can directly affect the induction length during detonation diffraction which determines the shock reflection strength. The dif作者: 挑剔為人 時間: 2025-3-22 16:42 作者: 挑剔為人 時間: 2025-3-22 20:24 作者: 不透明性 時間: 2025-3-22 23:35
Jessica L. Dillon,Laura J. Tafespecific impulse. With the growth of the specific mass flow rate of reactive mixture, the operation process, on the one hand, becomes more stable, and on the other hand, the number of detonation waves simultaneously rotating in one direction in the combustor annulus increases. The results of DLRE fi作者: AGATE 時間: 2025-3-23 03:18 作者: 開花期女 時間: 2025-3-23 07:13
Grasiella A. Andriani,Cristina Montagnames, which is discovered to be the main reason leading to the discrepancies between the previous similar studies. The width of the bifurcation channel is also critical as it can directly affect the induction length during detonation diffraction which determines the shock reflection strength. The dif作者: Hyaluronic-Acid 時間: 2025-3-23 11:55
2197-9529 logy.Includes up-to-date reviews and research results of det.This book focuses on the latest developments in detonation engines for aerospace propulsion, with a focus on the rotating detonation engine (RDE). State-of-the-art research contributions are collected from international leading researchers作者: 廣告 時間: 2025-3-23 15:41 作者: DUCE 時間: 2025-3-23 18:23
Brennan Decker,Lynette M. Shollous Spin Detonation (CSD) and a few essential facts from the prior publications. Furthermore, a summarization of the Continuous Detonation Wave Rocket Engine (CDWRE) concepts is examined. At long last, a detailed numerical investigation and experiment work of RDE is also presented.作者: CORE 時間: 2025-3-23 23:53 作者: 憤慨點(diǎn)吧 時間: 2025-3-24 04:21
https://doi.org/10.1007/978-1-4939-7280-7nitiation method, particle path, thermodynamic performance, shock wave reflections near the head-wall, spontaneously formation of multiple detonation waves, etc. In this chapter, we also discussed several recent examples of progress and accomplishments.作者: BIAS 時間: 2025-3-24 09:59 作者: somnambulism 時間: 2025-3-24 13:37 作者: foliage 時間: 2025-3-24 15:05 作者: RODE 時間: 2025-3-24 20:50
Pulse Detonation Cycle at Kilohertz Frequency,6 Hz. Under the condition of 1010 Hz operation, the total pressure of supplying oxidizer were varied. As the results, it was found that the DDT distance and time decreased by approximately 50% when the total pressure of supplying oxidizer increased by 242%.作者: 取回 時間: 2025-3-25 00:06 作者: 沒收 時間: 2025-3-25 05:01 作者: abolish 時間: 2025-3-25 10:35
Review on the Research Progresses in Rotating Detonation Engine,ous Spin Detonation (CSD) and a few essential facts from the prior publications. Furthermore, a summarization of the Continuous Detonation Wave Rocket Engine (CDWRE) concepts is examined. At long last, a detailed numerical investigation and experiment work of RDE is also presented.作者: 吞沒 時間: 2025-3-25 11:49 作者: synovial-joint 時間: 2025-3-25 17:56
Brennan Decker,Lynette M. Shollressure preheated air supply system was constructed which allows to supply air at rate of a few kg/s, preheated to more than 100?°C and at initial pressure up to 2.5?bar. Supply system for Jet-A fuel which could be preheated to 170?°C was also constructed. Additionally gaseous hydrogen supply system作者: 不怕任性 時間: 2025-3-25 20:56
Jessica L. Dillon,Laura J. Tafeerformed to examine the impact of the DLRE configuration and fuel supply parameters on the operation process and thrust performance. In experiments, the absolute pressures of NG and oxygen supply were up to 30 and 15?atm, respectively; the mass flow rate of the reactive mixture was varied from 0.05 作者: Ptsd429 時間: 2025-3-26 02:20 作者: faculty 時間: 2025-3-26 06:12
Marie-Lisa Eich,George J. Nettoormed using the detailed chemistry model. The comparison of the MUSCL and the 5th-order RWCNS (WCNS5MN) indicates that the shock front and the contact surface for the WCNS5MN can be improved with the better resolution than those for the MUSCL and that both rotating velocities are approximately 97% o作者: Madrigal 時間: 2025-3-26 09:05 作者: Ophthalmologist 時間: 2025-3-26 16:21
https://doi.org/10.1007/978-1-4939-7280-7ity was the first to conduct numerical and experimental research of the CDE in China. We designed several types of CDE combustion chambers and carried out experiments to verify its feasibility. In addition, we have performed a series of two- and three-dimensional simulations of the CDE. Numerical st作者: 切掉 時間: 2025-3-26 19:25 作者: 過渡時期 時間: 2025-3-26 23:18
Grasiella A. Andriani,Cristina Montagnadetonation research facilities in Temasek Laboratories. The main objective is to understand the re-initiation mechanisms through shock reflections, and investigate the performance of detonation re-initiation at different test conditions. Stable and unstable detonation waves are both taken into consi作者: Solace 時間: 2025-3-27 02:04 作者: 音樂戲劇 時間: 2025-3-27 07:06
978-3-319-88679-4Springer International Publishing AG 2018作者: 機(jī)械 時間: 2025-3-27 10:44 作者: preservative 時間: 2025-3-27 17:22 作者: oracle 時間: 2025-3-27 18:56
Detonation Control for Propulsion978-3-319-68906-7Series ISSN 2197-9529 Series E-ISSN 2197-9537 作者: 食草 時間: 2025-3-28 01:40
Performance of Rotating Detonation Engines for Air Breathing Applications,Laboratory’s Detonation Engine Research Facility. The performance scaling characteristics observed between various physical device configurations is discussed; included is the influence of mass flow rate, air injection area ratio and nozzle area ratio. The impact of geometry on the unsteady nature o作者: 思想流動 時間: 2025-3-28 02:16
Development of Gasturbine with Detonation Chamber,ressure preheated air supply system was constructed which allows to supply air at rate of a few kg/s, preheated to more than 100?°C and at initial pressure up to 2.5?bar. Supply system for Jet-A fuel which could be preheated to 170?°C was also constructed. Additionally gaseous hydrogen supply system作者: Ccu106 時間: 2025-3-28 09:51
Flow Structure in Rotating Detonation Engine with Separate Supply of Fuel and Oxidizer: Experiment erformed to examine the impact of the DLRE configuration and fuel supply parameters on the operation process and thrust performance. In experiments, the absolute pressures of NG and oxygen supply were up to 30 and 15?atm, respectively; the mass flow rate of the reactive mixture was varied from 0.05 作者: Ischemic-Stroke 時間: 2025-3-28 12:05 作者: machination 時間: 2025-3-28 15:03
Numerical Simulation on Rotating Detonation Engine: Effects of Higher-Order Scheme,ormed using the detailed chemistry model. The comparison of the MUSCL and the 5th-order RWCNS (WCNS5MN) indicates that the shock front and the contact surface for the WCNS5MN can be improved with the better resolution than those for the MUSCL and that both rotating velocities are approximately 97% o作者: 思考 時間: 2025-3-28 19:46 作者: Granular 時間: 2025-3-28 23:59 作者: cunning 時間: 2025-3-29 04:28
Pulse Detonation Cycle at Kilohertz Frequency,A novel semi-valveless PDC method, in which the inner diameter of the oxidizer feed line is equal to that of the combustor, can increase the pressure of detonable mixture by increasing total pressure of supplying oxidizer. In demonstration experiments, ethylene as fuel, pure oxygen as the oxidizer a
