Relevant bibliographies by topics / Jet flow

Contents

  1. Journal articles
  2. Dissertations / Theses
  3. Books
  4. Book chapters
  5. Conference papers
  6. Reports

Academic literature on the topic 'Jet flow'

Author: Grafiati
Published: 4 June 2021
Last updated: 7 September 2023

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Journal articles on the topic "Jet flow"

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Sugimoto, M., T. Shakouchi, K. Hayakawa, M. Okazaki, and M. Izawa. "Particle Laden Impinging Jet Flow from Rectangular Nozzle and Abrasive Jet Machining(Multiphase Flow 2)." Proceedings of the International Conference on Jets, Wakes and Separated Flows (ICJWSF) 2005 (2005): 325–30. http://dx.doi.org/10.1299/jsmeicjwsf.2005.325.

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Tabata, Takahide, Satoshi Someya, and Masahiro Nakashima. "JET FLOW ISSUING UPWARD WITH SUBSTANCE DIFFUSION(Jet and Plume)." Proceedings of the International Conference on Jets, Wakes and Separated Flows (ICJWSF) 2005 (2005): 399–404. http://dx.doi.org/10.1299/jsmeicjwsf.2005.399.

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Narabayashi, Tadashi, Yukitaka Yamazaki, Hidetoshi Kobayashi, and Toshihiko Shakouchi. "Flow Analysis for Single and Multi-Nozzle Jet Pump(Multiple Jet)." Proceedings of the International Conference on Jets, Wakes and Separated Flows (ICJWSF) 2005 (2005): 267–72. http://dx.doi.org/10.1299/jsmeicjwsf.2005.267.

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Imao, Shigeki, Satoshi Kikuchi, Yasuaki Kozato, and Takayasu Hayashi. "FLOW CHARACTERISTICS OF PLANE WALL JET WITH SIDE WALLS ON BOTH SIDES(Wall Jet and Wall Flow)." Proceedings of the International Conference on Jets, Wakes and Separated Flows (ICJWSF) 2005 (2005): 73–78. http://dx.doi.org/10.1299/jsmeicjwsf.2005.73.

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Okita, Yuji, Katsutaka Nakamura, Yuuta Shiizaki, and Daisuke Nobuta. "LASER OBSERVATION ON THE INNER FLOW STRUCTURE OF WATER JETS(Water Jet)." Proceedings of the International Conference on Jets, Wakes and Separated Flows (ICJWSF) 2005 (2005): 337–42. http://dx.doi.org/10.1299/jsmeicjwsf.2005.337.

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Liffman, K., and A. Siora. "Magnetosonic jet flow." Monthly Notices of the Royal Astronomical Society 290, no. 4 (1997): 629–35. http://dx.doi.org/10.1093/mnras/290.4.629.

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Peng, Guoyi. "NUMERICAL STUDY OF CAVITATING VORTEX FLOW IN STARTING SUBMERGED WATER JET(Water Jet)." Proceedings of the International Conference on Jets, Wakes and Separated Flows (ICJWSF) 2005 (2005): 355–60. http://dx.doi.org/10.1299/jsmeicjwsf.2005.355.

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Toshihiko, SHAKOUCHI, IRIYAMA Shota, KAWASHIMA Yuki, TSUJIMOTO Koichi, and ANDO Toshitake. "1012 FLOW CHARACTERISTICS OF SUBMERGED FREE JET FLOW FROM PETAL-SHAPED NOZZLE." Proceedings of the International Conference on Jets, Wakes and Separated Flows (ICJWSF) 2013.4 (2013): _1012–1_—_1012–6_. http://dx.doi.org/10.1299/jsmeicjwsf.2013.4._1012-1_.

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Mizuki, Kito, Shakouchi Toshihiko, Tsujimoto Koichi, and Ando Toshitake. "1002 RESONANCE JET FLOW FROM NOTCHED ORIFICE NOZZLE." Proceedings of the International Conference on Jets, Wakes and Separated Flows (ICJWSF) 2013.4 (2013): _1002–1_—_1002–6_. http://dx.doi.org/10.1299/jsmeicjwsf.2013.4._1002-1_.

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Tatsuya, Ishii, Enomoto Shunji, Nakamura Satoru, and Ishikawa Hitoshi. "1172 JET FLOW CONTROL USING A CLAW MIXER." Proceedings of the International Conference on Jets, Wakes and Separated Flows (ICJWSF) 2013.4 (2013): _1172–1_—_1172–6_. http://dx.doi.org/10.1299/jsmeicjwsf.2013.4._1172-1_.

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Dissertations / Theses on the topic "Jet flow"

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Miller, Adam Cole. "Flow control via synthetic jet actuation." Texas A&M University, 2004. http://hdl.handle.net/1969.1/1409.

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An experimental investigation was undertaken to determine the ability of Synthetic Jet Actuators to control the aerodynamic properties of a wing. The Synthetic Jet Actuator (SJA) was placed at two separate positions on a wing comprised of a NACA0015 airfoil. The first of the jet positions is located at 12% of the chord, hereby referred to as the leading edge Synthetic Jet Actuator. The second exit position is located at 99% chord of an airfoil and hereby is referred to as the trailing edge Synthetic Jet Actuator. The two locations produced different benefits as the angle of attack of the wing was increased. The leading edge Synthetic Jet Actuator delayed the onset of stall of an airfoil, suppressing stall up to 25 degrees angle of attack. The control of the aerodynamic characteristics was achieved by influencing the amount of the separated flowfield region. The effects of the dynamic stall vortex were investigated with wind tunnel testing during the pitching motion of an airfoil to determine how the flow reacts dynamically. The trailing edge synthetic jet actuator was investigated as a form of low angle “hingeless” control. The study investigated the effect of the jet momentum coefficient on the ability of the synthetic jet to modify the lifting and pitching moment produced from the wind tunnel model. The data indicates that, with the present implementation, the SJA-jet flap generates moderate lift and moment coefficient increments that should be suitable for hinge- less control. It was also shown that, for the current experimental setup and a given jet momentum coefficient, continuous blowing is more effective than oscillatory blowing/sucking. The data shows that combining the SJA with a Gurney flap does not result in performance enhancement.
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Tyagi, Ashok K. "Jet to jet impingement in a confined space." Thesis, National Library of Canada = Bibliothèque nationale du Canada, 1997. http://www.collectionscanada.ca/obj/s4/f2/dsk2/ftp02/NQ30117.pdf.

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Sanders, John E. "Jet dispersion in channels." Thesis, University of East London, 1998. http://roar.uel.ac.uk/1254/.

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This is an experimental and theoretical investigation of the dispersion of a round water jet discharging at various angles into a rectangular channel. A fundamental study of the jet is not only essential for a better understanding of the flow conditions produced by confined water jets but for a scientific approach to the design of hydraulic structures and to determine an efficient form of stilling basin for high velocity discharge from pipe outlets. The Laser Doppler Anemometry (LDA) technique was adapted for measurement of mean velocities and turbulence characteristics,, without any interference in the flow, and was utilised for the investigation of the complex three dimensional circulating flow which was experienced in the channel. In the experiments the inclination of the jet was varied from 45 to 90 degrees to the bed of the channel, while differing ratios of channel width and depth to jet diameter were studied for various Froude numbers. Detailed measurements of velocity decay, normal and lateral velocity profiles, distributions of pressure and turbulence characteristics have been carried out for selected flow conditions relating to the 45 degree oblique and vertical jet in order to determine the flow pattern and head dissipations. The experimental results have been analysed and compared with Glauert Is theory for a radial wall jet as a first approximation neglecting gravity forces when small compared with turbulent forces. Based on these results erosion experiments and model studies using a solid apron and a sand bed downstream, have been conducted to predict the minimum size of an efficient stilling basin and dimensions of any required blocks. Finally generalised design guide-lines and a standard code of practice have been developed for a stilling basin with high velocity pipe outlets. The research work will provide practical information and design procedures for consultants and other organisations working on the design and maintenance of a variety of water projects both in the UK and overseas.
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Ashforth-Frost, Shirley. "Flow visualisation of semi-confined jet impingement." Thesis, Nottingham Trent University, 1994. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.385846.

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Luo, Xinfu. "Plasma based jet actuators for flow control." Thesis, University of Southampton, 2012. https://eprints.soton.ac.uk/348870/.

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A set of plasma based jet actuators were designed for flow control applications. The characteristics of these actuators and their flow control applications were studied experimentally in a low speed wind tunnel. A dielectric barrier discharge (DBD) based jet actuator is designed, which is made of a covered cavity with two spanwise aligned parallel slots. Two-component particle image velocimetry (PIV) measurements were conducted to determine the effect of actuator in quiescent air and on a canonical zero pressure gradient turbulent boundary layer. It was found that the designed plasma jet actuator produced a transverse jet similar to a continuously blowing jet but with no mass addition into the flow field. The device is different from a traditional alternative blowing-and-suction synthetic jet as the current jet is continuously blown. As such, the DBD based jet actuator is different from either a mass injection blowing jet actuator or a traditional diaphragm based synthetic jet actuator. The impact of the actuation with the designed actuator on the boundary layer characteristics was investigated in detail at different Reynolds numbers. Circular cylinder wake flow control using a newly designed five-electrode plasma jet actuator is also presented in this thesis. This plasma actuator configuration mounted on the cylinder model can easily produce either a downward or upward jet into the flow around the circular cylinder by simply adjusting the same five electrodes’ electrical circuits. The experiments were performed at Reynolds numbers from 7,000 to 24,000. Wake profile measurements were made to evaluate the modification to the mean and fluctuation velocities in the cylinder wake. The results shown that the cylinder wake flow and the turbulence levels in the wake were modified under the actuations, sectional drag reduction and drag increment were obtained by different actuator actuation directions. The study suggested that this new designed five-electrode actuator can be applied to practical separation suppression or enhancement control by adjusting the plasma actuator electric circuits conveniently.
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Wells, Adam Joseph. "Experimental investigation of an airfoil with co-flow jet flow control." [Gainesville, Fla.] : University of Florida, 2005. http://purl.fcla.edu/fcla/etd/UFE0011656.

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Santhanakrishnan, Arvind. "CHARACTERIZATION AND FLOW PHYSICS OF PLASMA SYNTHETIC JET ACTUATORS." UKnowledge, 2007. http://uknowledge.uky.edu/gradschool_diss/545.

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Plasma synthetic jet actuators are investigated experimentally, in which the geometrical design of single dielectric barrier discharge (SDBD) plasma actuators is modified to produce zero-mass flux jets similar to those created by mechanical devices. The SDBD plasma actuator consists of two rectangular electrodes oriented asymmetrically and separated by a layer of dielectric material. Under an input of high voltage, high frequency AC or pulsed DC, a region of plasma is created in the interfacial air gap on account of electrical breakdown of the ambient air. A coupling between the electric field in the plasma and the neutral air near the actuator is introduced, such that the latter experiences a net force which results in a horizontal wall jet. This effect of the actuator has been demonstrated to be useful in mitigating boundary layer separation in aerodynamic flows. To increase the impact that a plasma actuator may have on the flow field, this research investigates the development and characterization of a novel flow control device, the plasma synthetic jet actuator, which tailors the residual air in the form of a vertical jet resembling conventional continuous and synthetic jets. This jet can be either three dimensional using annular electrode arrays, or nearly two dimensional using two rectangular strip exposed electrodes and one embedded electrode. Detailed measurements on the isolated plasma synthetic jet reveal that pulsed operation of the actuator results in the formation of multiple counterrotating vortical structures in the flow field. The output jet velocity and momentum are found to be higher for unsteady pulsing as compared to steady operation. In the case of flow over a flat plate, the actuator is observed to create a localized interaction region within which the baseline flow direction and boundary layer characteristics are modified. The efficiency of the actuator in coupling momentum to the neutral air is found to be related to the plasma morphology, pulsing frequency, actuator dimension, and input power. An analytical scaling model is proposed to describe the effects of varying the above variables on the output jet characteristics and actuator efficiency, and the experimental data is used for model validation.
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Smith, Matthew James. "The Analysis and Prediction of Jet Flow and Jet Noise about Airframe Surfaces." Thesis, Virginia Tech, 2013. http://hdl.handle.net/10919/23897.

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Aircraft noise mitigation has been an ongoing challenge for the aeronautics research community. In response to this challenge, aircraft concepts have been developed in which the propulsion system is integrated with the airframe to shield the noise from the observer. These concepts exhibit situations where the jet exhaust interacts with an airframe surface. Jet flows interacting with nearby surfaces exhibit a complex behavior in which acoustic and aerodynamic characteristics are altered. The physical understanding and accurate modeling of these characteristics are essential to designing future low-noise aircraft. In this thesis, an alternative approach is created for predicting jet mixing noise that utilizes an acoustic analogy and the solution of the steady Reynolds-Averaged Navier-Stokes (RANS) equations using a two equation turbulence model. A tailored Green's function is used in conjunction with the acoustic analogy to account for the propagation effects of mixing noise due to a nearby airframe surface. The tailored Green's function is found numerically using a newly developed ray tracing method. The variation of the aerodynamics, acoustic source, and far- field acoustic intensity are examined as a large flat plate is moved relative to the nozzle exit. Steady RANS solutions are used to study the aerodynamic changes in the field-variables and turbulence statistics. To quantify the propulsion airframe aeroacoustic (PAA) installation effects on the aerodynamic source, a non-dimensional number is formed that can be used as a basic guide to determine if the aerodynamic source is affected by the airframe and if additional noise produced by the airframe surface is present. The aerodynamic and noise prediction models are validated by comparing results with Particle Image Velocimetry (PIV) and far-field acoustic data respectively. The developed jet noise scattering methodology is then used to demonstrate the shielding effects of the Hybrid Wing Body (HWB) aircraft. The validation assessment shows that the acoustic analogy and tailored Green's function provided by the ray tracing method are capable of capturing jet shielding characteristics for multiple configurations and jet exit conditions.<br>Master of Science
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Garcia, Robert Gordon. "CFD simulation of flow fields associated with high speed jet impingement on deflectors." Thesis, Virginia Tech, 2007. http://hdl.handle.net/10919/31675.

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Computational Fluid Dynamics is used to analyze the formation of under-expanded jets and to investigate the three-dimensional flow field associated with the impingement of free jets onto stationary deflectors. This investigation was performed to develop a verified modeling ability for such problems. Predictions were compared with the experimental results obtained by Donaldson and Snedeker [1]. Computational models for free and impinging jets were created according to the data provided in Ref. 1. Numerical results for each of the experiments performed in this benchmark report are presented. <p> Three different turbulent free jets produced by a simple convergent nozzle were analyzed. These include a subsonic jet with p<sub>1</sub>/pâ =1 and M<sub>1</sub>=0.57, a moderately under-expanded jet with p<sub>1</sub>/pâ =1.42 and M<sub>1</sub>=1, and a highly under-expanded jet with p<sub>1</sub>/pâ =3.57 and M<sub>1</sub>=1. The reflecting shocks associated with the moderately under-expanded jet as well as the shock disk associated with the highly under-expanded jet were fully resolved. Velocity profile data predicted at locations downstream of the nozzle exit agreed very well with the experimental results. <p>The impingement of a moderately under-expanded jet with p<sub>1</sub>/pâ =1.42 and M<sub>1</sub>=1 was also investigated. The interaction of the high speed jet with circular flat plates at angles of 60° and 45° relative to the center axis of the jet are presented. Wall jet velocity profiles on the surface of the flat plate are fully resolved and compare well with experimental results. The CFD solver controls and method used to obtain these results are summarized and justified.<br>Master of Science
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Konduri, Indu Mohan. "Flow characteristics of jet fans in mines : experimental and numerical modeling /." Diss., This resource online, 1996. http://scholar.lib.vt.edu/theses/available/etd-06062008-152159/.

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Books on the topic "Jet flow"

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H, Swan D., and United States. National Aeronautics and Space Administration., eds. Rectangular subsonic jet flow field measurements. National Aeronautics and Space Administration, 1990.

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Tillman, T. G. Enhanced mixing of supersonic jets. American Institute of Aeronautics and Astronautics, 1988.

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Mankbadi, Reda R. Effects of core turbulence on jet excitability. Institute for Computational Mechanics in Propulsion, 1988.

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United States. National Aeronautics and Space Administration., ed. Unsteady jet flow computation towards noise prediction. National Aeronautics and Space Administration, 1994.

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North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Computational and experimental assessment of jets in cross flow: Papers presented and discussions recorded at the Fluid Dynamics Panel Symposium held in Winchester, United Kingdom, from 19th-22nd April 1993. AGARD, 1993.

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North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Computational and experimental assessment of jets in crossflow. AGARD, 1993.

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J, Morris Philip, and United States. National Aeronautics and Space Administration., eds. Supersonic coaxial jet noise predictions. National Aeronautics and Space Administration, 1995.

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United States. National Aeronautics and Space Administration., ed. Dropsize correlation for cryogenic liquid-jet atomization. NASA, 1991.

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Institute for Computer Applications in Science and Engineering., ed. Modeling jets in cross flow. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1994.

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Lepicovsky, J. Coherent large-scale structures in high Reynolds number supersonic jets. Lockheed-Georgia Company, 1985.

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Book chapters on the topic "Jet flow"

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Makarenko, T. M., T. U. Volnova, T. N. Bezmenova, and V. I. Ribakov. "Subsonic Jet Visualization." In Flow Visualization VI. Springer Berlin Heidelberg, 1992. http://dx.doi.org/10.1007/978-3-642-84824-7_20.

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Peng, Xiaofeng. "Jet Flow Phenomena." In Micro Transport Phenomena During Boiling. Springer Berlin Heidelberg, 2010. http://dx.doi.org/10.1007/978-3-642-13454-8_4.

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Shintani, Ryuji, and Atsushi Okajima. "Visualization of Sub-Nozzle Jet of Air Jet Looms." In Flow Visualization VI. Springer Berlin Heidelberg, 1992. http://dx.doi.org/10.1007/978-3-642-84824-7_22.

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Pirumov, Ul’yan G., and Gennadi S. Roslyakov. "Nozzles of Jet Engines." In Gas Flow in Nozzles. Springer Berlin Heidelberg, 1986. http://dx.doi.org/10.1007/978-3-642-86790-3_5.

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Panigrahi, Pradipta Kumar, and Krishnamurthy Muralidhar. "Imaging Jet Flow Patterns." In Imaging Heat and Mass Transfer Processes. Springer New York, 2012. http://dx.doi.org/10.1007/978-1-4614-4791-7_5.

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Decher, Reiner. "Pressure: The Bernoulli Principle and Flow Energy Conservation." In The Vortex and The Jet. Springer Singapore, 2022. http://dx.doi.org/10.1007/978-981-16-8028-1_5.

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AbstractThe relation between descriptive variables of flowing air, pressure and the like, and the dynamic field, speeds or velocities, are often invoked for their understanding. Such relationships depend on whether the flow is compressible or not. When it is, physical work done by air elements on one another, become important. This chapter, virtually devoid of illuminating images, nevertheless sheds light on how to think about air flows in general and how to deduce the local pressures from knowledge of the flow field.
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Kolev, Nikolay Ivanov. "Liquid and gas jet disintegration." In Multiphase Flow Dynamics 2. Springer Berlin Heidelberg, 2011. http://dx.doi.org/10.1007/978-3-642-20598-9_10.

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Bulat, O. V., V. V. Golub, V. N. Lyakhov, and A. M. Shulmeister. "Interaction Between Impulse Jet and Flat Plate." In Flow Visualization VI. Springer Berlin Heidelberg, 1992. http://dx.doi.org/10.1007/978-3-642-84824-7_25.

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Amitay, Michael, and Ari Glezer. "Aerodynamic Flow Control Using Synthetic Jet Actuators." In Control of Fluid Flow. Springer Berlin Heidelberg, 2006. http://dx.doi.org/10.1007/978-3-540-36085-8_2.

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Sun, Mingbo, Hongbo Wang, and Feng Xiao. "Flow Structures of Gaseous Jet in Supersonic Crossflow." In Jet in Supersonic Crossflow. Springer Singapore, 2019. http://dx.doi.org/10.1007/978-981-13-6025-1_3.

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Conference papers on the topic "Jet flow"

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Dano, Bertrand, Danah Kirk, and Gecheng Zha. "Experimental Investigation of Jet Mixing Mechanism of Co-Flow Jet Airfoil." In 5th Flow Control Conference. American Institute of Aeronautics and Astronautics, 2010. http://dx.doi.org/10.2514/6.2010-4421.

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Tamburello, David, and Michael Amitay. "Manipulation of an Axisymmetric Jet Using a Single Perpendicular Control Jet." In 3rd AIAA Flow Control Conference. American Institute of Aeronautics and Astronautics, 2006. http://dx.doi.org/10.2514/6.2006-3700.

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Guo, Dahai, Andrew Cary, and Ramesh Agarwal. "Numerical Simulation of Vectoring Control of a Primary Jet with a Synthetic Jet." In 1st Flow Control Conference. American Institute of Aeronautics and Astronautics, 2002. http://dx.doi.org/10.2514/6.2002-3284.

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Pack Melton, LaTunia G., Mehti Koklu, Marlyn Andino, John C. Lin, and Louis M. Edelman. "Sweeping Jet Optimization Studies." In 8th AIAA Flow Control Conference. American Institute of Aeronautics and Astronautics, 2016. http://dx.doi.org/10.2514/6.2016-4233.

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Tang, Gongyu, and Ramesh K. Agarwal. "Numerical Simulation of Flow Control Over NASA Hump with Uniform Blowing Jet and Synthetic Jet." In 2018 Flow Control Conference. American Institute of Aeronautics and Astronautics, 2018. http://dx.doi.org/10.2514/6.2018-4017.

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Kamran, Muhammad, and James McGuirk. "Active Control of a Mach 0.9 Jet Using Steady and Pulsed Control Jets." In 4th Flow Control Conference. American Institute of Aeronautics and Astronautics, 2008. http://dx.doi.org/10.2514/6.2008-3880.

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LEPICOVSKY, J., K. AHUJA, W. BROWN, and P. MORRIS. "Acoustic control of free jet mixing." In Shear Flow Control Conference. American Institute of Aeronautics and Astronautics, 1985. http://dx.doi.org/10.2514/6.1985-569.

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Sinha, A., S. Balasubramanian, and S. Gopalakrishanan. "Internal and external characteristics of a superheated jet." In MULTIPHASE FLOW 2015. WIT Press, 2015. http://dx.doi.org/10.2495/mpf150201.

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MANKBADI, REDA, EDWARD RICE, and GANESH RAMAN. "Effects of core turbulence on jet excitability." In 2nd Shear Flow Conference. American Institute of Aeronautics and Astronautics, 1989. http://dx.doi.org/10.2514/6.1989-966.

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Crittenden, Tom. "Combustion Powered Pulsed Jet Actuators and Applications." In 4th Flow Control Conference. American Institute of Aeronautics and Astronautics, 2008. http://dx.doi.org/10.2514/6.2008-4424.

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Reports on the topic "Jet flow"

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Elcrat, A. Ideal Jet Flow in Two Dimensions. Defense Technical Information Center, 1989. http://dx.doi.org/10.21236/ada208275.

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Hook, Anson, Martin Jankowiak, and Jay G. Wacker. Jet Dipolarity: Top Tagging with Color Flow. Office of Scientific and Technical Information (OSTI), 2011. http://dx.doi.org/10.2172/1022564.

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Kerschen, Edward J. Receptivity Theory in Compressible Jet Flow Control. Defense Technical Information Center, 1997. http://dx.doi.org/10.21236/ada325563.

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Orkwis, Paul D., Matteo Pes, Claudio Filz, et al. Characterization and Modeling of Synthetic Jet Flow Fields. Defense Technical Information Center, 2005. http://dx.doi.org/10.21236/ada433145.

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Smith, Douglas R. Synthetic Jet Flow Control in a Matched-Index-of-Refraction Flow Facility. Defense Technical Information Center, 2010. http://dx.doi.org/10.21236/ada563071.

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Wu, J. M., A. D. Vakili, and F. M. Yu. Investigation of Non-Symmetric Jets in Cross Flow (Discrete Wing Tip Jet Effects). Defense Technical Information Center, 1986. http://dx.doi.org/10.21236/ada179783.

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Jeffrey B. Parker and John A. Krommes. Zonal Flow as Pattern Formation: Merging Jets and the Ultimate Jet Length Scale. Office of Scientific and Technical Information (OSTI), 2013. http://dx.doi.org/10.2172/1062392.

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KOCH, M. R. Guidance for Flow Computer Setup on the Jet Pump Motor Recirculation Flow Line. Office of Scientific and Technical Information (OSTI), 2000. http://dx.doi.org/10.2172/801354.

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Glezer, Ari. Shear Flow Control Using Synthetic Jet Fluidic Actuator Technology. Defense Technical Information Center, 1999. http://dx.doi.org/10.21236/ada368201.

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Lewis, B. E., and H. J. Marquess. Evaluation of a commercially available low-flow steam jet. Office of Scientific and Technical Information (OSTI), 1986. http://dx.doi.org/10.2172/5350397.

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