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Journal articles on the topic 'Jet interaction'

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1

Solsjo, R., M. Jangi, C. Chartier, O. Andersson, and X. S. Bai. "HC1-3 Jet-Jet Interaction in Diesel Engine Combustion(HC: HCCI Combustion,General Session Papers)." Proceedings of the International symposium on diagnostics and modeling of combustion in internal combustion engines 2012.8 (2012): 398–403. http://dx.doi.org/10.1299/jmsesdm.2012.8.398.

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2

Raman, Ganesh, Edmane Envia, and Timothy J. Bencic. "Jet-Cavity Interaction Tones." AIAA Journal 40, no. 8 (2002): 1503–11. http://dx.doi.org/10.2514/2.1845.

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3

Cassel, Louis A. "Applying Jet Interaction Technology." Journal of Spacecraft and Rockets 40, no. 4 (2003): 523–37. http://dx.doi.org/10.2514/2.3992.

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4

Jordan, Peter, Vincent Jaunet, Aaron Towne, et al. "Jet–flap interaction tones." Journal of Fluid Mechanics 853 (August 23, 2018): 333–58. http://dx.doi.org/10.1017/jfm.2018.566.

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Motivated by the problem of jet–flap interaction noise, we study the tonal dynamics that occurs when an isothermal turbulent jet grazes a sharp edge. We perform hydrodynamic and acoustic pressure measurements to characterise the tones as a function of Mach number and streamwise edge position. The observed distribution of spectral peaks cannot be explained using the usual edge-tone model, in which resonance is underpinned by coupling between downstream-travelling Kelvin–Helmholtz wavepackets and upstream-travelling sound waves. We show, rather, that the strongest tones are due to coupling betwe
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5

Raman, G., E. Envia, and T. J. Bencic. "Jet-cavity interaction tones." AIAA Journal 40 (January 2002): 1503–11. http://dx.doi.org/10.2514/3.15224.

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6

SZUMOWSKI, A., G. SOBIERAJ, W. SELEROWICZ, and J. PIECHNA. "STARTING JET–WALL INTERACTION." Journal of Sound and Vibration 232, no. 4 (2000): 695–702. http://dx.doi.org/10.1006/jsvi.1999.2772.

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7

Lopez, J. Javier, and Lyle M. Pickett. "Jet/wall interaction effects on soot formation in a diesel fuel jet(Measurement PM in Flames)." Proceedings of the International symposium on diagnostics and modeling of combustion in internal combustion engines 2004.6 (2004): 387–94. http://dx.doi.org/10.1299/jmsesdm.2004.6.387.

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8

Lai, Adrian C. H., and Joseph H. W. Lee. "Dynamic interaction of multiple buoyant jets." Journal of Fluid Mechanics 708 (August 10, 2012): 539–75. http://dx.doi.org/10.1017/jfm.2012.332.

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AbstractAn array of closely spaced round buoyant jets interact dynamically due to the pressure field induced by jet entrainment. Mutual jet attraction can result in a significant change in jet trajectories. Jet merging also leads to overlapping of the passive scalar fields associated with the individual jets, resulting in mixing characteristics that are drastically different from those of an independent free jet. A general semi-analytical model for the dynamic interaction of multiple buoyant jets in stagnant ambient conditions is proposed. The external irrotational flow field induced by the bu
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9

KOJIMA, Tadatomo, and Yoshihiro MATSUOKA. "Interaction Characteristics of Supersonic Jet." Journal of the Visualization Society of Japan 11, Supplement2 (1991): 27–30. http://dx.doi.org/10.3154/jvs.11.supplement2_27.

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10

Margaris, P., D. Marles, and I. Gursul. "Experiments on jet/vortex interaction." Experiments in Fluids 44, no. 2 (2007): 261–78. http://dx.doi.org/10.1007/s00348-007-0399-7.

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11

Torres-Albà, Núria, and Valentí Bosch-Ramon. "Gamma rays from red giant wind bubbles entering the jets of elliptical host blazars." Astronomy & Astrophysics 623 (March 2019): A91. http://dx.doi.org/10.1051/0004-6361/201833697.

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Context. Blazars in elliptical hosts have a population of red giants surrounding their jet. These stars can carry large wind-blown bubbles into the jets, leading to gamma-ray emission through bubble-jet interactions. Aims. We study the interaction dynamics and the gamma-ray emission produced when the bubbles formed by red giant winds penetrate the jet of a blazar in an elliptical galaxy. Methods. First, we characterized the masses and penetration rates of the red giant wind bubbles that enter the jet. Then, the dynamical evolution of these bubbles under the jet impact was analysed analytically
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12

PERUCHO, MANEL. "JET PROPAGATION AND DECELERATION." International Journal of Modern Physics: Conference Series 28 (January 2014): 1460165. http://dx.doi.org/10.1142/s2010194514601653.

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Extragalactic jets in active galactic nuclei (AGN) are divided into two morphological types, namely Fanaroff-Riley I (FRI) and Fanaroff-Riley II (FRII). The former show decollimated structure at the kiloparsec scales and are thought to be decelerated by entrainment within the first kiloparsecs of evolution inside the host galaxy. The entrainment and deceleration can be, at least partly, due to the interaction of jets with stellar winds and gas clouds that enter in the jet as they orbit around the galactic centre. In this contribution, I review recent simulations to study the dynamic effect of
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13

Waterman, Stephanie, Nelson G. Hogg, and Steven R. Jayne. "Eddy–Mean Flow Interaction in the Kuroshio Extension Region." Journal of Physical Oceanography 41, no. 6 (2011): 1182–208. http://dx.doi.org/10.1175/2010jpo4564.1.

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Abstract The authors use data collected by a line of tall current meter moorings deployed across the axis of the Kuroshio Extension (KE) jet at the location of maximum time-mean eddy kinetic energy to characterize the mean jet structure, the eddy variability, and the nature of eddy–mean flow interactions observed during the Kuroshio Extension System Study (KESS). A picture of the 2-yr record mean jet structure is presented in both geographical and stream coordinates, revealing important contrasts in jet strength, width, vertical structure, and flanking recirculation structure. Eddy variability
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14

Tamburello, David A., and Michael Amitay. "Interaction of a free jet with a perpendicular control jet." Journal of Turbulence 8 (January 2007): N21. http://dx.doi.org/10.1080/14685240601007078.

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15

Luo, Shi-Jie, Yao-Feng Liu, and Yu-Wei Liu. "Visualization of asymmetric separation induced by lateral jet interaction on a slender body in supersonic flow." International Journal of Modern Physics B 34, no. 14n16 (2020): 2040081. http://dx.doi.org/10.1142/s0217979220400810.

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The lateral jet interaction on a slender body in supersonic flow was investigated by numerical simulation. The spatial and surface flow characteristics induced by jet interaction were shown. As a result, when the lateral jet is not in the longitudinal symmetry plane, the jet interaction causes asymmetric separation flow of surface and space, and destroys the pressure distributions of the slender body. With different angle of attack and circumferential positions of jet, the flow characteristic of the after body for jet in asymmetry plane changes greatly. The results with and without jet interac
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16

Peña Fernández, Juan José, and Jörn Sesterhenn. "Compressible starting jet: pinch-off and vortex ring–trailing jet interaction." Journal of Fluid Mechanics 817 (March 27, 2017): 560–89. http://dx.doi.org/10.1017/jfm.2017.128.

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The dominant feature of the compressible starting jet is the interaction between the emerging vortex ring and the trailing jet. There are two types of interaction: the shock–shear layer–vortex interaction and the shear layer–vortex interaction. The former is clearly not present in the incompressible case, since there are no shocks. The shear layer–vortex interaction has been reported in the literature in the incompressible case and it was found that compressibility reduces the critical Reynolds number for the interaction. Four governing parameters describe the compressible starting jet: the no
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17

Araudo, A. T., V. Bosch-Ramon, and G. E. Romero. "Radiation from matter entrainment in astrophysical jets: the AGN case." Proceedings of the International Astronomical Union 6, S275 (2010): 131–35. http://dx.doi.org/10.1017/s1743921310015802.

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AbstractJets are found in a variety of astrophysical sources. In all the cases the jet propagates with a supersonic velocity through the external medium, which can be inhomogeneous, and inhomogeneities could penetrate into the jet. The interaction of the jet material with an obstacle produces a bow-like shock within the jet in which particles can be accelerated up to relativistic energies and emit high-energy photons. In this work, we explore the active galactic nuclei scenario, focusing on the dynamical and radiative consequences of the interaction at different jet heights. We find that the p
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18

Luo, Shi Jie. "Asymmetrical Lateral Jet Interaction on a Slender Body in Supersonic Flow." Applied Mechanics and Materials 565 (June 2014): 107–12. http://dx.doi.org/10.4028/www.scientific.net/amm.565.107.

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The lateral jet interaction on a slender body with rudders in supersonic flow had been investigated by numerical simulation, when the lateral jet is not in the longitudinal symmetry plane. It was called Asymmetrical lateral jet interaction in this paper. The flow features of jet interaction flowfield on the surface of the body or in the space far from the surface at different angles of attack and total pressure of jet was analyzed. As a result, the lateral jet interaction disturbed the pressure distributions of the slender body, and it was divided into near-field interaction near jet and far-f
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19

Desikan, S. L. N., B. Murugan, K. Srinivasan, and S. Sajan. "Twin Jet Interaction and Reverse Flow." Journal of Spacecraft and Rockets 52, no. 6 (2015): 1577–85. http://dx.doi.org/10.2514/1.a33309.

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20

Chen, Jin, Yaofeng Liu, and Jinglong Bo. "Numerical Simulation of Lateral Jet Interaction." Journal of Applied Mathematics and Physics 05, no. 09 (2017): 1686–93. http://dx.doi.org/10.4236/jamp.2017.59141.

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21

Schweigert, I., S. Vagapov, L. Lin, and M. Keidar. "Plasma Jet Interaction with Dielectric Surface." Journal of Physics: Conference Series 1112 (November 2018): 012004. http://dx.doi.org/10.1088/1742-6596/1112/1/012004.

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22

Kinzel, M., M. Moeny, M. Krane, and I. Kirschner. "Jet-Supercavity Interaction: Insights from CFD." Journal of Physics: Conference Series 656 (December 3, 2015): 012133. http://dx.doi.org/10.1088/1742-6596/656/1/012133.

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23

Moeny, M. J., M. H. Krane, I. N. Kirschner, and M. P. Kinzel. "Jet-Supercavity Interaction: Insights from Experiments." Journal of Physics: Conference Series 656 (December 3, 2015): 012162. http://dx.doi.org/10.1088/1742-6596/656/1/012162.

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24

OKAMOTO, TETSUSHI, MIKI YAGITA, AKIRA WATANABE, and KOSEI KAWAMURA. "INTERACTION OF TWIN TURBULENT CIRCULAR JET." Bulletin of JSME 28, no. 238 (1985): 617–22. http://dx.doi.org/10.1299/jsme1958.28.617.

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25

Lomer, W. M. "Experiences of wall interaction in JET." Journal of Nuclear Materials 133-134 (August 1985): 18–24. http://dx.doi.org/10.1016/0022-3115(85)90106-0.

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26

Chan, Philemon C., Kit K. Kan, and James H. Stuhmiller. "A Computational Study of Bubble-Structure Interaction." Journal of Fluids Engineering 122, no. 4 (2000): 783–90. http://dx.doi.org/10.1115/1.1319157.

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The complex interaction between underwater explosion bubbles and nearby structures is studied using two-fluid computational fluid dynamics. Gravitational effects on bubble jetting are significantly different between jet-up and jet-down orientations. This paper presents computational results of underwater explosion bubble dynamics near a disk and a sphere. The results show that the bubble jetting and collapse phenomena and the consequent pressure loading are affected by the structure’s shape, the orientation of the bubble to the structure, and the bubble depth. A unifying notion emerges connect
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27

Sandham, Neil D., and Adriana M. Salgado. "Nonlinear interaction model of subsonic jet noise." Philosophical Transactions of the Royal Society A: Mathematical, Physical and Engineering Sciences 366, no. 1876 (2008): 2745–60. http://dx.doi.org/10.1098/rsta.2008.0049.

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Noise generation in a subsonic round jet is studied by a simplified model, in which nonlinear interactions of spatially evolving instability modes lead to the radiation of sound. The spatial mode evolution is computed using linear parabolized stability equations. Nonlinear interactions are found on a mode-by-mode basis and the sound radiation characteristics are determined by solution of the Lilley–Goldstein equation. Since mode interactions are computed explicitly, it is possible to find their relative importance for sound radiation. The method is applied to a single stream jet for which expe
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28

Hadadpour, Ahmad, Mehdi Jangi, and Xue Song Bai. "Jet-jet interaction in multiple injections: A large-eddy simulation study." Fuel 234 (December 2018): 286–95. http://dx.doi.org/10.1016/j.fuel.2018.07.010.

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29

PERUCHO, M., and V. BOSCH-RAMON. "STUDYING THE INTERACTION BETWEEN MICROQUASAR JETS AND THEIR ENVIRONMENTS." International Journal of Modern Physics D 17, no. 10 (2008): 1939–45. http://dx.doi.org/10.1142/s0218271808013601.

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In high-mass microquasars (HMMQ), strong interactions between jets and stellar winds at binary system scales could occur. In order to explore this possibility, we have performed numerical two-dimensional hydrodynamical simulations of jets crossing the dense stellar material to study how the jet will be affected by these interactions. We find that the jet head generates strong shocks in the wind. These shocks reduce the jet advance speed, and compress and heat up the jet and wind material. In addition, strong recollimation shocks can occur where pressure balance between the jet side and the sur
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30

Laouedj, Samir, Juan P. Solano, and Abdelylah Benazza. "Synthetic jet cross-flow interaction with orifice obstruction." International Journal of Numerical Methods for Heat & Fluid Flow 25, no. 4 (2015): 749–61. http://dx.doi.org/10.1108/hff-01-2014-0013.

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Purpose – The purpose of this paper is to describe the flow structure and the time-resolved and time-mean heat transfer characteristics in the interaction between a synthetic jet and a cross flow, when an obstruction reduces the cross-section of the orifice where the jet is formed. Design/methodology/approach – The microchannel flow interacted by the pulsed jet is modeled using a two-dimensional finite volume simulation with unsteady Reynolds-averaged Navier-Stokes equations while using the Shear-Stress-Transport (SST) k-ω turbulence model to account for fluid turbulence. Findings – The comput
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31

Sorokin, Evgeniy, Igor Khramtsov, and Evgeniya Cherenkova. "EXPERIMENTAL STUDY OF INFLUENCE OF THE CHEVRONS ON JET-FLAP INTERACTION NOISE." Akustika 32 (March 1, 2019): 189–94. http://dx.doi.org/10.36336/akustika201932189.

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The interaction noise of turbulent jet with deflected flap is considered. The test objects are small-scale models of turbulent jet and flap in scale 1:6. To compare the effect of chevrons on the interaction noise level, experiments are carried out for two types of conical nozzles: conventional and chevron. It is also used conventional flap and chevron flap. Noise measurements in acoustic far field are carried out in the PNRUP acoustic chamber for directions from 15 to 105 degrees with a step of 15 degrees. The flap deflection angle varied from 0 to 45 degrees in increments of 5 degrees. The re
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32

del Palacio, S., V. Bosch-Ramon, and G. E. Romero. "Gamma rays from jets interacting with BLR clouds in blazars." Astronomy & Astrophysics 623 (March 2019): A101. http://dx.doi.org/10.1051/0004-6361/201834231.

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Context. The innermost parts of powerful jets in active galactic nuclei are surrounded by dense, high-velocity clouds from the broad-line region, which may penetrate into the jet and lead to the formation of a strong shock. Such jet-cloud interactions are expected to have measurable effects on the γ-ray emission from blazars. Aims. We characterise the dynamics of a typical cloud-jet interaction scenario, and the evolution of its radiative output in the 0.1–30 GeV energy range, to assess to what extent these interactions can contribute to the γ-ray emission in blazars. Methods. We use semi-anal
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33

Aldabbagh, L. B. Y., I. Sezai, and A. A. Mohamad. "Three-Dimensional Investigation of a Laminar Impinging Square Jet Interaction With Cross-Flow." Journal of Heat Transfer 125, no. 2 (2003): 243–49. http://dx.doi.org/10.1115/1.1561815.

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The flow and heat transfer characteristics of an impinging laminar square jet through cross-flow have been investigated numerically by using the three-dimensional Navier-Stokes and energy equations in steady state. The simulations have been carried out for jet to cross-flow velocity ratios between 0.5 and 10 and for nozzle exit to plate distances between 1D and 6D, where D is the jet width. The complex nature of the flow field featuring a horseshoe vortex has been investigated. The calculated results show that the flow structure is strongly affected by the jet-to-plate distance. In addition, f
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34

Li, Long-Fei, Jiang-Feng Wang, Fa-Ming Zhao, and Yu-Han Wang. "Numerical study of interaction between jet with rudders on slender body at hypersonic condition." Modern Physics Letters B 32, no. 12n13 (2018): 1840019. http://dx.doi.org/10.1142/s0217984918400195.

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In this paper, a numerical study of the interaction between transverse cold jets on slender body in front of or between X-shape rudders with rudders in the oncoming free stream is presented. Firstly, the flow field at different jet conditions is simulated and analyzed. Then, the total force and moment amplification factors of the corresponding slender body with jet at different locations are analyzed and compared with those results of non-jet flow. Numerical results show that interactions take a great effect to the configuration of the flow field around rudders and the pressure distribution on
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35

Vieyro, F. L., V. Bosch-Ramon, and N. Torres-Albà. "Non-thermal emission resulting from a supernova explosion inside an extragalactic jet." Astronomy & Astrophysics 622 (February 2019): A175. http://dx.doi.org/10.1051/0004-6361/201833319.

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Context. Core-collapse supernovae are found in galaxies with ongoing star-formation. In a starburst galaxy hosting an active galactic nucleus with a relativistic jet, supernovae can take place inside the jet. The collision of the supernova ejecta with the jet flow is expected to lead to the formation of an interaction region, in which particles can be accelerated and produce high-energy emission. Aims. We study the non-thermal radiation produced by electrons accelerated as a result of a supernova explosion inside the jet of an active galactic nucleus within a star-forming galaxy. Methods. We f
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36

Viti, Valerio, Scott Wallis, Joseph A. Schetz, Reece Neel, and R. D. W. Bowersox. "Jet Interaction with a Primary Jet and an Array of Smaller Jets." AIAA Journal 42, no. 7 (2004): 1358–68. http://dx.doi.org/10.2514/1.4850.

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37

Li, Zhi-wei, Wen-xin Huai, and Jie Han. "Large Eddy Simulation of the Interaction Between Wall Jet and Offset Jet." Journal of Hydrodynamics 23, no. 5 (2011): 544–53. http://dx.doi.org/10.1016/s1001-6058(10)60148-5.

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38

Kang, Kyoung Tai, and Soogab Lee. "Modeling and Assessment of Jet Interaction Database for Continuous-Type Side Jet." Journal of Spacecraft and Rockets 54, no. 4 (2017): 916–29. http://dx.doi.org/10.2514/1.a33807.

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39

Suzuki-Vidal, F., M. Bocchi, S. V. Lebedev, et al. "Jet-ambient interaction of a supersonic, radiatively-cooled jet in laboratory experiments." EAS Publications Series 58 (2012): 127–31. http://dx.doi.org/10.1051/eas/1258020.

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40

Luo, Shi Jie, Yao Feng Liu, and Ning Cao. "Numerical Simulation of Lateral Jet Interaction a Slender Body in Supersonic Flow." Applied Mechanics and Materials 404 (September 2013): 296–301. http://dx.doi.org/10.4028/www.scientific.net/amm.404.296.

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A numerical investigation has been conducted to research the interaction flowfield of lateral jet not in the longitudinal symmetry plane on a slender body with rudders in supersonic flow. The surface and space flow features of jet interaction flowfield with different angles of attack was analyzed. The paper also compared with and without jet interaction flowfield characteristics. As a result, the jet interaction destroys pressure distributions of the slender body, and causes normal and lateral loads. With angle of attack, the pressure distributions of the after body and rudders surfaces are ch
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41

Parmar, Harisinh, Vishnu Pareek, Chi M. Phan, and Geoffrey M. Evans. "Influence of jet–jet interaction on droplet size and jet instability in immiscible liquid–liquid system." Chemical Engineering Science 123 (February 2015): 247–54. http://dx.doi.org/10.1016/j.ces.2014.11.015.

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42

Shang, J. S., D. L. McMaster, N. Scaggs, and M. Buck. "Interaction of jet in hypersonic cross stream." AIAA Journal 27, no. 3 (1989): 323–29. http://dx.doi.org/10.2514/3.10115.

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43

Wlezien, R. W. "Nozzle geometry effects on supersonic jet interaction." AIAA Journal 27, no. 10 (1989): 1361–67. http://dx.doi.org/10.2514/3.10272.

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44

Hassan, Ez, John Boles, Hikaru Aono, Douglas Davis, and Wei Shyy. "Supersonic jet and crossflow interaction: Computational modeling." Progress in Aerospace Sciences 57 (February 2013): 1–24. http://dx.doi.org/10.1016/j.paerosci.2012.06.002.

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45

Lai, Adrian C. H., and Joseph H. W. Lee. "Multiple tandem jet interaction in a crossflow." Journal of Hydrodynamics 22, S1 (2010): 616–20. http://dx.doi.org/10.1016/s1001-6058(10)60007-8.

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46

Kashimura, Hideo, Tsuyoshi Yasunobu, and Yumiko Otobe. "Interaction between Underexpanded Supersonic Jet and Obstacle." International Journal of Aeroacoustics 12, no. 5-6 (2013): 539–50. http://dx.doi.org/10.1260/1475-472x.12.5-6.539.

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47

Chen, Shuxing, and Aifang Qu. "Interaction of rarefaction waves in jet stream." Journal of Differential Equations 248, no. 12 (2010): 2931–54. http://dx.doi.org/10.1016/j.jde.2010.03.004.

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48

Jing, Li, Liu Zhenxia, and Xiao Hong. "Simulation and Experimental Validation of Jet Interaction." Journal of Computational and Theoretical Nanoscience 12, no. 4 (2015): 613–18. http://dx.doi.org/10.1166/jctn.2015.3775.

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49

Algwari, Qais Th, and Deborah O'Connell. "Plasma Jet Interaction With a Dielectric Surface." IEEE Transactions on Plasma Science 39, no. 11 (2011): 2368–69. http://dx.doi.org/10.1109/tps.2011.2160658.

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50

Gauthier, E., P. Andrew, G. Arnoux, Y. Corre, and H. Roche. "Plasma wall interaction during ELMs in JET." Journal of Nuclear Materials 363-365 (June 2007): 1026–31. http://dx.doi.org/10.1016/j.jnucmat.2007.01.262.

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