標題: Titlebook: Experimental Methods of Shock Wave Research; Ozer Igra,Friedrich Seiler Book 2016 Springer International Publishing Switzerland 2016 Exper [打印本頁] 作者: Localized 時間: 2025-3-21 16:05
書目名稱Experimental Methods of Shock Wave Research影響因子(影響力)
書目名稱Experimental Methods of Shock Wave Research影響因子(影響力)學科排名
書目名稱Experimental Methods of Shock Wave Research網(wǎng)絡(luò)公開度
書目名稱Experimental Methods of Shock Wave Research網(wǎng)絡(luò)公開度學科排名
書目名稱Experimental Methods of Shock Wave Research被引頻次
書目名稱Experimental Methods of Shock Wave Research被引頻次學科排名
書目名稱Experimental Methods of Shock Wave Research年度引用
書目名稱Experimental Methods of Shock Wave Research年度引用學科排名
書目名稱Experimental Methods of Shock Wave Research讀者反饋
書目名稱Experimental Methods of Shock Wave Research讀者反饋學科排名
作者: sparse 時間: 2025-3-22 00:11
Shock Wave Experiments in a High-Temperature Gas Flowc-heated wind tunnel is one of these facilities and features long operational time; thus the arc-heated wind tunnel has been used mainly for the development and evaluation of a thermal protection system for space transportation systems. Thus generated plasma flows can be employed for the experiments作者: Mere僅僅 時間: 2025-3-22 01:51 作者: 殺人 時間: 2025-3-22 05:00
The Aachen Shock Tunnel TH2 with Dual Driver Mode Operationitions. Their performance range mainly depends on their driver technology which can be distinguished between conventional driver, employing pre-compressed gas, combustion and detonation driver and free piston driver. In principle, the highest performance in terms of nozzle reservoir pressure and tem作者: 流眼淚 時間: 2025-3-22 09:59 作者: 復習 時間: 2025-3-22 16:57 作者: 復習 時間: 2025-3-22 17:51 作者: 細節(jié) 時間: 2025-3-22 21:59 作者: ZEST 時間: 2025-3-23 03:55
Shock Tunnels and Hypersonic Research in IISc, Bangalorededicated centre for the research, among other domains of fluid dynamics, on the shock dominated phenomena. More often than not, the focus of the research is on the flow phenomena at high enthalpies, which are addressed using the impulse facilities—shock tubes and tunnels. Ever since its inception a作者: figure 時間: 2025-3-23 07:56
Gun TunnelsGun tunnels produce low enthalpy hypersonic flows with durations of several tens of milliseconds. For a capital investment similar to that of a comparably-sized, regular shock tunnel, gun tunnels offer at least an order of magnitude longer flow duration. This makes gun tunnels an attractive option f作者: characteristic 時間: 2025-3-23 09:49 作者: 暴行 時間: 2025-3-23 15:05
Hypersonic Ludwieg Tubelunt and slender configurations. Furthermore, in order to enable testing of laminar and turbulent flows, the facility should provide a Reynolds-number of 20 Million, based on the model length. The test time should be in the order of 100 ms in order to allow for a range of useful flow measurement tec作者: RECUR 時間: 2025-3-23 20:00
Ozer Igra,Friedrich SeilerWell structured encyclopedic book.Presents a state-of the art overview on Experimental methods of Shock Wave Research.Vol. 9 of the Shock Waves Science and Technology Reference Library.Includes supple作者: RALES 時間: 2025-3-24 02:08
Shock Wave Science and Technology Reference Libraryhttp://image.papertrans.cn/e/image/318879.jpg作者: 最初 時間: 2025-3-24 05:41
Vicente Cortés,Klaus Kr?ncke,Jan LouisA shock tube is a facility that can produce transmitted shock waves in controlled laboratory conditions. The facility is a duct divided into two sections as shown schematically in Fig.?1. One part, the driver, accommodates high pressure gas (P.) while the other section (the driven) contains the low pressure test gas (P.).作者: GUILT 時間: 2025-3-24 09:55 作者: REP 時間: 2025-3-24 14:25 作者: Introduction 時間: 2025-3-24 17:20
Development of the New Piston-Driven Shock-Tunnel HELMThe simulation of high enthalpy, hypersonic flows is a field of continued research efforts and provides a difficult task despite all progress made in the past years.作者: 難聽的聲音 時間: 2025-3-24 22:02 作者: 收到 時間: 2025-3-24 23:45 作者: 難取悅 時間: 2025-3-25 06:38 作者: 保存 時間: 2025-3-25 09:03
Hidetaka Hamada,Mihai Iancu,Gabriela Kohrc-heated wind tunnel is one of these facilities and features long operational time; thus the arc-heated wind tunnel has been used mainly for the development and evaluation of a thermal protection system for space transportation systems. Thus generated plasma flows can be employed for the experiments作者: 反省 時間: 2025-3-25 12:22 作者: archaeology 時間: 2025-3-25 16:10
Dorina Mitrea,Irina Mitrea,Marius Mitreaitions. Their performance range mainly depends on their driver technology which can be distinguished between conventional driver, employing pre-compressed gas, combustion and detonation driver and free piston driver. In principle, the highest performance in terms of nozzle reservoir pressure and tem作者: 吝嗇性 時間: 2025-3-25 20:13
Dorina Mitrea,Irina Mitrea,Marius Mitreaterceptors, re-entry vehicles and projectiles and to their related steering systems. The main and great advantage of using shock tunnels for aerothermodynamic investigations is the reproduction of real flight conditions of vehicles at a very low cost. This chapter is dedicated to measurement methods作者: 某人 時間: 2025-3-26 00:46
https://doi.org/10.1007/978-3-031-31561-9e fluid molecules occur. Due to the extremely high power requirement and the severe flow environment, the required test conditions can only be achieved in ground based impulse facilities. The most successful types of facility which are able to generate high enthalpy and high pressure hypersonic flow作者: IST 時間: 2025-3-26 08:18
https://doi.org/10.1007/978-981-16-0147-7ronment characterized by strong shocks and high temperatures, and the flow in the hypersonic regime behaves quite differently from that at supersonic Mach numbers (Bertin in Hypersonic Aerothermodynamics. Washington DC, .; Park in Nonequilibrium Hypersonic Aerothermodynamics, Wiley, New York, .; And作者: 滔滔不絕地說 時間: 2025-3-26 09:26 作者: hankering 時間: 2025-3-26 15:09
Alfonso Zamora Saiz,Ronald A. Zú?iga-Rojasdedicated centre for the research, among other domains of fluid dynamics, on the shock dominated phenomena. More often than not, the focus of the research is on the flow phenomena at high enthalpies, which are addressed using the impulse facilities—shock tubes and tunnels. Ever since its inception a作者: Immunization 時間: 2025-3-26 18:31 作者: foodstuff 時間: 2025-3-26 23:10 作者: 殘酷的地方 時間: 2025-3-27 04:06
A. Hamiltonian and Lagrangian formalisms,lunt and slender configurations. Furthermore, in order to enable testing of laminar and turbulent flows, the facility should provide a Reynolds-number of 20 Million, based on the model length. The test time should be in the order of 100 ms in order to allow for a range of useful flow measurement tec作者: muscle-fibers 時間: 2025-3-27 08:48
Alfonso Zamora Saiz,Ronald A. Zú?iga-Rojastly contributed to the fundamental understanding of many aspects of high speed/shock dominated flows and their control. The present chapter describes the various shock tunnels in the laboratory and reviews some of the important research works carried out in these ground test facilities.作者: Bronchial-Tubes 時間: 2025-3-27 11:00
Shock Tunnels and Hypersonic Research in IISc, Bangaloretly contributed to the fundamental understanding of many aspects of high speed/shock dominated flows and their control. The present chapter describes the various shock tunnels in the laboratory and reviews some of the important research works carried out in these ground test facilities.作者: Condense 時間: 2025-3-27 14:33
Measurement of the Physical Properties of Blast Wavesers; passive techniques such as the deflection or fracture?of plastic or brittle cantilevers; time-of-arrival records of the primary shock front, and high-speed time-resolved photography of shock fronts and flow tracers within the blast wave.作者: Flounder 時間: 2025-3-27 19:19 作者: 潛伏期 時間: 2025-3-28 00:08
Development and Calibration of Detonation-Driven High-Enthalpy and Hypersonic Test FacilitiesMach numbers (Bertin in Hypersonic Aerothermodynamics. Washington DC, .; Park in Nonequilibrium Hypersonic Aerothermodynamics, Wiley, New York, .; Anderson in Hypersonic and High Temperature Gas Dynamics. McGraw-Hill Book Company, New York, .).作者: Psa617 時間: 2025-3-28 04:51 作者: COMMA 時間: 2025-3-28 07:47 作者: 四海為家的人 時間: 2025-3-28 10:43 作者: Cultivate 時間: 2025-3-28 16:02 作者: 細微的差異 時間: 2025-3-28 19:32 作者: 雄偉 時間: 2025-3-29 00:33
Shock Wave Experiments in a High-Temperature Gas FlowIn this chapter, a 20?kW-class arc-heated wind tunnel operated at Department of Aeronautics and Astronautics, Kyushu University is depicted and shock wave experiments in an arc-heated high-temperature flow are discussed.作者: spondylosis 時間: 2025-3-29 04:03 作者: conduct 時間: 2025-3-29 08:43 作者: 狂怒 時間: 2025-3-29 14:56
Hypersonic Ludwieg Tubes resulted in a specific wind tunnel configuration that meets these requirements. This is the hypersonic Ludwieg tube. Several of these gas dynamics facilities are in operation worldwide. The present contribution describes one of the successful designs of this kind, along with data that characterize the quality and capabilities of this facility.作者: guardianship 時間: 2025-3-29 18:02
ves Science and Technology Reference Library.Includes supple.This comprehensive and carefully edited volume presents a variety of experimental methods used in Shock Waves research. In 14 self contained chapters this 9.th. volume of the “Shock Wave Science and Technology Reference Library” presents t作者: Integrate 時間: 2025-3-29 21:41 作者: Landlocked 時間: 2025-3-30 01:50 作者: 大范圍流行 時間: 2025-3-30 05:22 作者: Diuretic 時間: 2025-3-30 10:28 作者: 強壯 時間: 2025-3-30 12:38 作者: 啤酒 時間: 2025-3-30 18:36
