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Relevant bibliographies by topics / Ram accelerators

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Academic literature on the topic 'Ram accelerators'

Author: Grafiati

Published: 4 June 2021

Last updated: 6 February 2022

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Journal articles on the topic "Ram accelerators"

1

Li, Chiping, K. Kailasanath, E. S. Oran, A. M. Landsberg, and J. P. Boris. "Dynamics of oblique detonations in ram accelerators." Shock Waves 5, no. 1-2 (June 1995): 97–101. http://dx.doi.org/10.1007/bf02425040.

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Higgins, Andrew J. "Ram Accelerators: Outstanding Issues and New Directions." Journal of Propulsion and Power 22, no. 6 (November 2006): 1170–87. http://dx.doi.org/10.2514/1.18209.

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Li, Chiping, K. Kailasanath, and Elaine S. Oran. "Stability of projectiles in thermally choked ram accelerators." Journal of Propulsion and Power 12, no. 4 (July 1996): 807–9. http://dx.doi.org/10.2514/3.24105.

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Yungster, S., K. Radhakrishnan, and M. J. Rabinowitz. "Reacting Flow Establishment in Ram Accelerators: A Numerical Study." Journal of Propulsion and Power 14, no. 1 (January 1998): 10–17. http://dx.doi.org/10.2514/2.5259.

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Li, Chiping, and K. Kailasanath. "Initiation Mechanism of Thermally Choked Combustion in Ram Accelerators." Journal of Propulsion and Power 15, no. 1 (January 1999): 151–53. http://dx.doi.org/10.2514/2.5404.

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Jasemi, Masoomeh, Shaahin Hessabi, and Nader Bagherzadeh. "Reliable and Energy Efficient MLC STT-RAM Buffer for CNN Accelerators." Computers & Electrical Engineering 86 (September 2020): 106698. http://dx.doi.org/10.1016/j.compeleceng.2020.106698.

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Rom, J. "Performance Limits for Projectile Flight in the Ram and External Propulsion Accelerators." Journal of Propulsion and Power 13, no. 5 (September 1997): 583–91. http://dx.doi.org/10.2514/2.5222.

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Brandies, Julius. "Use of jet interaction for ignition in ram and external propulsion accelerators." Journal of Propulsion and Power 11, no. 6 (November 1995): 1299–306. http://dx.doi.org/10.2514/3.23972.

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Legendre, J. F., M. Giraud, and P. Bauer. "Detonation properties of dense methane-oxygen-diluent gaseous mixtures: application to ram accelerators." Shock Waves 8, no. 5 (October 1, 1998): 267–73. http://dx.doi.org/10.1007/s001930050119.

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Nettleton, Michael A. "The applications of unsteady, multi-dimensional studies of detonation waves to ram accelerators." Shock Waves 10, no. 1 (March 1, 2000): 9–22. http://dx.doi.org/10.1007/s001930050175.

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Dissertations / Theses on the topic "Ram accelerators"

1

Chew, Gilbert. "Projectile nose heating in the Ram accelerator /." Thesis, Connect to this title online; UW restricted, 1995. http://hdl.handle.net/1773/9957.

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Brueckner, Frank Peter. "Finite element analysis of high-speed flows with application to the ram accelerator concept." Diss., The University of Arizona, 1991. http://hdl.handle.net/10150/185417.

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A Petrov-Galerkin method for the solution of the compressible Euler and Navier-Stokes equations is presented. The method is based on the introduction of an anisotropic balancing diffusion in the local direction of the propogation of the scalar variables. The direction in which the diffusion is added and its magnitude are automatically calculated locally using a criterion that is optimal for one-dimensional transport equations. Algorithms are developed using bilinear quadrilateral and linear triangular elements. The triangular elements are used in conjunction with an adaptive scheme using unstructured meshes. Several applications are presented that show the exceptional stability and accuracy of the method, including the ram accelerator concept for the acceleration of projectiles to ultrahigh velocities. Both two-dimensional and axisymmetric models are employed to evaluate multiple projectile configurations and flow conditions.

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Bundy, Christopher. "Effects of unsteady flow and real gas equations of state on high pressure ram accelerator operation /." Thesis, Connect to this title online; UW restricted, 2001. http://hdl.handle.net/1773/10008.

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4

Bargalló, Font Enric. "IFMIF accelerator facility RAMI analyses in the engineering design phase." Doctoral thesis, Universitat Politècnica de Catalunya, 2014. http://hdl.handle.net/10803/144657.

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The planned International Fusion Materials Irradiation Facility (IFMIF) has the mission to test and qualify materials for future fusion reactors. IFMIF will employ the deuteron-lithium stripping reaction to irradiate the test samples with a high-energy neutron flux. IFMIF will consist mainly of two linear deuteron accelerators, a liquid lithium loop and a test cell. Accelerated deuterons will collide with the lithium producing a high-energy neutron flux that will irradiate the material samples in the test cell. A timely and relevant fusion neutron source is essential in the path towards DEMO and future fusion power plants. For this reason, IFMIF is required to have high availability to obtain a fusion materials database to find suitable materials for DEMO design within the anticipated timeline. RAMI (Reliability Availability Maintainability Inspectability) analyses are being performed in the very early stages of design to meet such requirements. The IFMIF accelerator facility is composed of two independent linear accelerators, each of which produces a 40 MeV, 125 mA deuteron beam in a continuous wave mode at 175 MHz. These beam characteristics pose several unprecedented challenges: the highest beam intensity, the highest space charge, the highest beam power and the longest RFQ (Radio Frequency Quadrupole). As a result of these challenges, many design characteristics are counter to high-availability performance: the design is reluctant to accept failures, machine protection systems are likely to stop the beam undesirably, cryogenic components require long periods for maintenance, and activation of components complicates maintenance activities. These design difficulties, together with the high availability requirements and the demanding scheduled operational periods, make RAMI analysis an essential tool in the engineering design phase. These studies were performed in collaboration with system designers, enabling the creation of RAMI models that reflect current accelerator design. This feedback has been of the utmost importance to propose plausible design modifications in order to improve the availability performance of the machine. Parallel activity on the design and construction of the Linear IFMIF Prototype Accelerator (LIPAc) provided the detailed design information needed to conduct these studies properly. An iterative process was followed to match IFMIF design and availability studies. These iterations made it possible to include recommendations and design change proposals coming from the RAMI analyses into the accelerator reference design. Iterations consist of gathering information from the design, creating or updating the RAMI models, obtaining and analyzing results, and proposing ways to improve the design. Three different approaches were carried out in the iterative process. First, a comparison with other similar facilities was performed. Second, an individual fault tree analysis was developed for each system of the accelerator. Finally, a Monte Carlo simulation was performed for the whole accelerator facility considering synergies between systems. These approaches make it possible to go from detailed hardware availability analyses to global accelerator performance, to identify weak design points, and to propose design alternatives as well as foresee IFMIF performance, maintenance and operation characteristics. The IFMIF accelerator facility design was analyzed from the RAMI point of view, estimating its future availability and guiding the design towards a high reliability and availability performance. In order to achieve the high-availability requirements several design changes have already been included in the accelerator reference design whereas other important design modifications have been proposed and will be further analyzed in future design phases.

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Bengherbia, Tarek. "Contribution to numerical simulation analysis of the flow in the ram accelerator in the subdetonative propulsion mode." Chasseneuil-du-Poitou, Ecole nationale supérieure de mécanique et d'aéronautique, 2009. http://www.theses.fr/2009ESMA0019.

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L'accélérateur par effet stato en régime sous-détonatif, caractérisés par une vitesse du projectile inférieure à la célérité de la détonation dans le mélange considéré est, à l'heure actuelle, le mieux connu. La compréhension des phénomènes mis en jeu dans cette technologie est subordonnée à une importante étude expérimentale associée à la mise au point de moyens numériques. C'est l'objet du travail présenté dans ce mémoire qui décrit numériquement, à l'aide d'un code CFD de combustion turbulente, le processus de combustion qui s'opère autour du projectile. Les résultats, comparés aux données expérimentales existantes disponibles au Laboratoire de l'Université de Washington, ont permis de parfaire la fiabilité d'un code de calcul monodimensionnel en régime sousdétonatif. Les calculs analytiques font intervenir des équations d'état dont la validité est discutée. La poussée générée par l'accélérateur est calculée et les valeurs déduites de cette analyse 1D sont en excellent accord avec les expériences. Cette démarche a pour but d'apporter une contribution en termes de prédiction des performances de poussée d'un accélérateur à effet stato et de choix du mélange réactif optimal
The purpose of this work is to examine in details the flow field characteristics of the thermally choked ram accelerator using five step kinetic reaction mechanisms. The results from the simulations are compared with experimental values from representative experiments at the University of Washington 38-mm-bore facility. The data that were used for comparison with theory were derived from experiments performed in a 16-m-long tube with CH4/O2/N2 propellant mixtures at pressures on the order of several MPa. The data derived from these CFD calculations were used to implement a one-dimensional computer code which has been developed to predict the thrust in the thermally chocked combustion mode and is aimed at providing data over a wide range of initial pressures, where the steady state calculation is no longer valid and the real gas effects must be accounted for. This code includes both steady and unsteady state calculations, using several equations of state. The predicted thrust and velocity agree well with experimental values. The code, which requires simple data input and very low computer capabilities, provides an easy and rapid access to the prediction of the ram accelerator performance in the thermally choked combustion regime, over a wide range of mixture compositions and fill pressures

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Sasoh, Akihiro, In-Seuck Jeung, and Jeong-Yeol Choi. "Access to Space without Energy and Propellant on Board." American Institite of Physics, 2008. http://hdl.handle.net/2237/12050.

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Sasoh, Akihiro, Koichi Mori, Kohei Anju, Koji Suzuki, Masaya Shimono, and Keisuke Sawada. "Diagnostics and Impulse Performance of Laser-Ablative Propulsion." American Institite of Physics, 2008. http://hdl.handle.net/2237/12005.

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8

Chang, Ying-Li, and 張穎力. "Controlled Electron Injection In a Plasma-waveguide-based Laser Wakefield Accelerator By Implementation Of a Density Down Ramp." Thesis, 2012. http://ndltd.ncl.edu.tw/handle/40266242472822517972.

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碩士
國立中正大學
物理學系暨研究所
100
Laser wakefield electron accelerator has been demonstrated to have the capability of generating GeV-energy, low-emittance, high-stability electron pulses in centimeter scale length. It has shown great potential to become the key technology for next-generation TeV collider and various table-top ultrashort-pulse photon sources of wavelength ranging from THz to gamma-ray. These applications require an electron beam with high quality and stability, both of which are determined by finely controlled injection and acceleration processes in a laser-driven plasma wave. Here we report demonstration of production of a low-energy-spread electron beam via injection by longitudinal wave-breaking induced in a density down ramp in a plasma waveguide. In this scheme, the plasma waveguide is generated by using the axicon-ignitor-heater scheme, and an additional transverse heater pulse passing through a knife edge is used to produce longitudinal density variation in the plasma waveguide. This technique allows us to freely control the position and slope of the density ramp and to observe them with probing interferometry. It was observed that generation of a high-energy quasi-monoenergetic electron beam occurs only when the transverse heater pulse produces a density down ramp, and the probability of production varies with the position of density ramp. Good guiding of the pump laser pump was still maintained under the condition of presence of density ramps and high pump-pulse energy. The energy spread of the produced electron beam can be as low as 1%. The tunability of the density ramp allows us to clarify the ramp injection process and to optimize the quality of the electron beam. With this technique of fabrication of three-dimensional plasma density structure, integration of electron injector, accelerator, and x-ray free-electron laser in a single plasma waveguide may be achieved.

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Books on the topic "Ram accelerators"

1

Takayama, K., and A. Sasoh, eds. Ram Accelerators. Berlin, Heidelberg: Springer Berlin Heidelberg, 1998. http://dx.doi.org/10.1007/978-3-642-46876-6.

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2

Takayama, K. Ram Accelerators: Proceedings of the Third International Workshop on Ram Accelerators Held in Sendai, Japan, 16-18 July 1997. Berlin, Heidelberg: Springer Berlin Heidelberg, 1998.

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1940-, Takayama K., and Sasoh A, eds. Ram accelerators: Proceedings of the Third International Workshop on Ram Accelerators, held in Sendai, Japan, 16-18 July 1997. Berlin: Springer, 1998.

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4

International Workshop on Ram Accelerators (4th 1999 Poitiers, France). RAMAC-IV: Proceedings : Fourth International Workshop on Ram Accelerators : ENSMA--University of Poitiers, France, September 13-17, 1999. [Paris, France]: EDP Sciences, 2000.

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5

Bruckner, A. P. Investigation of advanced propulsion technologies: The RAM accelerator and the flowing gas radiation heater, NASA grant no. NAG 1-1288, final report, 1 July 1991 - 30 June 1992. Seattle, WA: Aerospace and Energetics Research Program, Dept. of Aeronautics, University of Washington, FL-10, 1992.

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6

Aarnio, Michael. Design of a ram accelerator mass launch system. Seattle, Wash: Dept. of Aeronautics and Astronautics, University of Washington, 1988.

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7

Soetrisno, Moeljo. Simulation of the flow field of a ram accelerator. Washington, D. C: American Institute of Aeronautics and Astronautics, 1991.

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8

Kruczynski, David L. Analysis of ram acceleration for high velocity applications. Aberdeen Proving Ground, Maryland: Ballistic Research Laboratory, 1991.

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9

Bruckner, A. P. Investigation of hypersonic ramjet propulsion cycles using a ram accelerator test facility. Paris, France: International Astronautical Federation, 1991.

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10

Chuck, C. Combusting flow simulations of detonation and shock-induced combustion waves for ram accelerator configurations with viscous effect. Washington, D. C: American Institute of Aeronautics and Astronautics, 1991.

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Book chapters on the topic "Ram accelerators"

1

Knowlen, C., and A. Sasoh. "Ram accelerator performance modeling." In Ram Accelerators, 25–37. Berlin, Heidelberg: Springer Berlin Heidelberg, 1998. http://dx.doi.org/10.1007/978-3-642-46876-6_2.

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Kruczynski, D. L. "High performance ram accelerator research." In Ram Accelerators, 97–104. Berlin, Heidelberg: Springer Berlin Heidelberg, 1998. http://dx.doi.org/10.1007/978-3-642-46876-6_8.

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Matsuo, A. "Numerical prediction of envelope oscillation phenomena of shock-induced combustion." In Ram Accelerators, 271–78. Berlin, Heidelberg: Springer Berlin Heidelberg, 1998. http://dx.doi.org/10.1007/978-3-642-46876-6_27.

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Bruckner, A. P. "The ram accelerator: overview and state of the art." In Ram Accelerators, 3–23. Berlin, Heidelberg: Springer Berlin Heidelberg, 1998. http://dx.doi.org/10.1007/978-3-642-46876-6_1.

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5

Sasoh, A., S. Hirakata, J. Maemura, Y. Hamate, and K. Takayama. "Thermally choked operation in a 25-mm-bore ram accelerator." In Ram Accelerators, 111–18. Berlin, Heidelberg: Springer Berlin Heidelberg, 1998. http://dx.doi.org/10.1007/978-3-642-46876-6_10.

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Sen, Liu, Z. Y. Bai, H. X. Jian, X. H. Ping, and S. Q. Bu. "37-mm bore ram accelerator of CARDC." In Ram Accelerators, 119–22. Berlin, Heidelberg: Springer Berlin Heidelberg, 1998. http://dx.doi.org/10.1007/978-3-642-46876-6_11.

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Buckwalter, D. L., C. Knowlen, and A. P. Bruckner. "Real gas effects on thermally choked ram accelerator performance." In Ram Accelerators, 125–34. Berlin, Heidelberg: Springer Berlin Heidelberg, 1998. http://dx.doi.org/10.1007/978-3-642-46876-6_12.

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Morales, M. M., M. A. S. Minucci, J. B. Channes, A. G. Ramos, and D. Bastos-Netto. "Numerical investigation on subdetonative mode ramjet-in-tube." In Ram Accelerators, 135–42. Berlin, Heidelberg: Springer Berlin Heidelberg, 1998. http://dx.doi.org/10.1007/978-3-642-46876-6_13.

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Wang, X. J., E. Spiegler, and Y. Timnat. "On the optimization of thermally-choked ram accelerator systems." In Ram Accelerators, 143–50. Berlin, Heidelberg: Springer Berlin Heidelberg, 1998. http://dx.doi.org/10.1007/978-3-642-46876-6_14.

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Seiler, F., F. Gatau, and G. Mathieu. "Prediction of surface heating of a projectile flying in RAMAC 30 of ISL." In Ram Accelerators, 151–58. Berlin, Heidelberg: Springer Berlin Heidelberg, 1998. http://dx.doi.org/10.1007/978-3-642-46876-6_15.

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Conference papers on the topic "Ram accelerators"

1

LI, C., K. KAILASANATH, and E. ORAN. "Stability of oblique detonations in RAM accelerators." In 30th Aerospace Sciences Meeting and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1992. http://dx.doi.org/10.2514/6.1992-89.

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Ghorbanian, Kaveh, and James Sterling. "Gas dynamic unstart in superdetonative ram accelerators." In 32nd Joint Propulsion Conference and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1996. http://dx.doi.org/10.2514/6.1996-2948.

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LI, CHIPING, K. KAILASANATH, E. ORAN, J. BORIS, and A. LANDSBERG. "Numerical simulations of transient flows in ram accelerators." In 29th Joint Propulsion Conference and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1993. http://dx.doi.org/10.2514/6.1993-1916.

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LI, CHIPING, K. KAILASANATH, E. ORAN, A. LANDSBERG, and J. BORIS. "Analysis of transient flows in thermally choked ram accelerators." In 29th Joint Propulsion Conference and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1993. http://dx.doi.org/10.2514/6.1993-2187.

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Li, Chiping, K. Kailasanath, and E. Oran. "Analysis of stability of projectiles in thermally choked ram accelerators." In 34th Aerospace Sciences Meeting and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1996. http://dx.doi.org/10.2514/6.1996-344.

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Li, Chiping, and K. Kailasanath. "Starting performance of thermally-choked ram accelerators at high mixture pressures." In 35th Joint Propulsion Conference and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1999. http://dx.doi.org/10.2514/6.1999-2950.

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Wang, Xiaojian. "Numerical study of design optimization and operational limits in superdetonative ram accelerators." In 35th Joint Propulsion Conference and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1999. http://dx.doi.org/10.2514/6.1999-2268.

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Rom, Josef. "On the acceleration of projectiles in the ram and external-propulsion accelerators by the energy balance analysis." In 32nd Joint Propulsion Conference and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1996. http://dx.doi.org/10.2514/6.1996-2951.

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Sasoh, A., Y. Hamate, G. Utsunomiya, and K. Takayama. "High acceleration ram accelerator operation." In 35th Joint Propulsion Conference and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1999. http://dx.doi.org/10.2514/6.1999-2262.

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Brandeis, J. "Ram accelerator utilizing active projectile." In 33rd Aerospace Sciences Meeting and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1995. http://dx.doi.org/10.2514/6.1995-288.

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Reports on the topic "Ram accelerators"

1

Hanson, R. K. Shock Tube Studies of Ram Accelerator Phenomena. Fort Belvoir, VA: Defense Technical Information Center, September 2000. http://dx.doi.org/10.21236/ada384344.

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Bruckner, Adam P., and Carl Knowlen. Investigation of Rapid Pressurization Techniques for the Ram Accelerator. Fort Belvoir, VA: Defense Technical Information Center, October 2003. http://dx.doi.org/10.21236/ada417707.

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Emma, Paul J. Accelerator Physics Challenges of X-Ray FEL SASE Sources. Office of Scientific and Technical Information (OSTI), May 2002. http://dx.doi.org/10.2172/799090.

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Jacob, J., M. Ong, and P. Wargo. Flash X-Ray (FXR) Accelerator Optimization Electronic Time-Resolved Measurement of X-Ray Source Size. Office of Scientific and Technical Information (OSTI), July 2005. http://dx.doi.org/10.2172/878193.

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Ong, M., T. Houck, B. Kreitzer, R. Paris, G. Vogtlin, and J. Zentler. FLASH X-RAY (FXR) LINEAR INDUCTION ACCELERATOR (LIA) OPTIMIZATION Sensor Delay Correction. Office of Scientific and Technical Information (OSTI), May 2006. http://dx.doi.org/10.2172/899421.

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Proctor, I. D., M. L. Roberts, J. E. McAninch, and G. S. Bench. Proof-of-concept development of PXAMS (projectile x-ray accelerator mass spectrometry). Office of Scientific and Technical Information (OSTI), March 1996. http://dx.doi.org/10.2172/221026.

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Gutjahr, A., F. Phillips, P. W. Kubik, and D. Elmore. An improved method for statistical analysis of raw accelerator mass spectrometry data. Office of Scientific and Technical Information (OSTI), January 1987. http://dx.doi.org/10.2172/6329593.

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Kroc, Thomas K. A Compact Superconducting RF Accelerator for Electron Beam and X-Ray Irradiation. Office of Scientific and Technical Information (OSTI), April 2018. http://dx.doi.org/10.2172/1508020.

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Ong, M., and G. Vogtlin. Flash X-Ray (FXR) Accelerator Optimization - Beam-induced Voltage Simulation and TDR Measurements. Office of Scientific and Technical Information (OSTI), April 2004. http://dx.doi.org/10.2172/15014170.

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Sanford, T. W. L., R. B. Spielman, and G. A. Chandler. Wire number doubling in plasma-shell regime increases Z-accelerator X-ray power. Office of Scientific and Technical Information (OSTI), December 1997. http://dx.doi.org/10.2172/554833.

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