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Relevant bibliographies by topics / Converging Diverging Nozzles

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Academic literature on the topic 'Converging Diverging Nozzles'

Author: Grafiati

Published: 4 June 2021

Last updated: 1 February 2022

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Journal articles on the topic "Converging Diverging Nozzles"

1

Mzad, Hocine, and Mohamed Elguerri. "Theoretical and Experimental Investigation of Compressible Flow through Convergent–Divergent Nozzles." Advanced Materials Research 452-453 (January 2012): 1277–85. http://dx.doi.org/10.4028/www.scientific.net/amr.452-453.1277.

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The present paper is concerned with the study of compressible flow in a converging-diverging nozzle. From a theoretical and experimental investigation of the flow in an illustrative channel with convergent-divergent area variation, the behavior of the flow along the channel was found to be generally similar in trend to the flow in a stationary convergent-divergent nozzle. In compressible flows, the density and temperature variations are often significant. Therefore, the following study provides additional information on shock location, Mach number behavior and pressure distribution by varying

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Acar, M., R. K. Turton, and G. R. Wray. "Air Flow in Yarn Texturing Nozzles." Journal of Engineering for Industry 109, no. 3 (1987): 197–202. http://dx.doi.org/10.1115/1.3187118.

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The air-jet texturing process, a purely mechanical means of texturing continuous filament yarns, is described. Industrial texturing nozzles are reviewed and categorized in two groups, either as converging-diverging or cylindrical type nozzles. A mathematical model is developed for the complex airflow in cylindrical type texturing nozzles, and experimental data obtained from various nozzles verify the flow predicted by this model. The mathematical model is also shown to be in good agreement with the data obtained from a modified experimental nozzle, which has a trumpet shaped diverging exit. Fu

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3

Flock, Andreas K., and Ali Gülhan. "Design of converging-diverging nozzles with constant-radius centerbody." CEAS Space Journal 12, no. 2 (2019): 191–201. http://dx.doi.org/10.1007/s12567-019-00286-4.

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AbstractSeveral flow phenomena, such as recirculating wake flows or noise generation, occur in aerodynamic configurations with backward facing steps. In this context, subsonic nozzles with constant-radius centerbodies exist, which enable fundamental research of these phenomena for $$M < 1$$M<1. For the supersonic regime, however, the existing database and knowledge are limited. Therefore, this work presents a design approach for a converging-diverging nozzle with constant-radius centerbody. For the nozzle throat, Sauer’s method is modified to include a centerbody. The method of character

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Bober, W., and W. L. Chow. "Nonideal Isentropic Gas Flow Through Converging-Diverging Nozzles." Journal of Fluids Engineering 112, no. 4 (1990): 455–60. http://dx.doi.org/10.1115/1.2909425.

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A method for treating nonideal gas flows through converging-diverging nozzles is described. The method incorporates the Redlich-Kwong equation of state. The Runge-Kutta method is used to obtain a solution. Numerical results were obtained for methane gas. Typical plots of pressure, temperature, and area ratios as functions of Mach number are given. From the plots, it can be seen that there exists a range of reservoir conditions that require the gas to be treated as nonideal if an accurate solution is to be obtained.

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Chavan, Kanchan, B. Bhingole, J. Raut, and A. B. Pandit. "Numerical Optimization of converging diverging miniature cavitating nozzles." Journal of Physics: Conference Series 656 (December 3, 2015): 012138. http://dx.doi.org/10.1088/1742-6596/656/1/012138.

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Shourehdeli, Shaban Alyari, Kamran Mobini, and Ali Asakereh. "Numerical Investigation of the Effects of Primary Nozzle Diverging Portion on Performance of the Supersonic Ejector of an Ejector Refrigeration Cycle." International Journal of Air-Conditioning and Refrigeration 27, no. 03 (2019): 1950030. http://dx.doi.org/10.1142/s2010132519500305.

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A supersonic ejector with desirable performance characteristics reduces the energy consumption rate of an ejector refrigeration system and increases its coefficient of performance (COP). In this paper, the effects of using different primary nozzles on the performance of a supersonic ejector of an ejector refrigeration system have been numerically studied, while the working fluid is steam. To this end, conical, Rao and parallel-flow primary nozzles with identical converging portions and equal exit area to throat area ratios have been tested. The diverging portion curves for the parallel-flow an

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Wilson, Erich A., Dan Adler, Benjamin Z. Bal-Or, Valery Sherbaum, and Michael Lichtsinder. "Optimizing Subcritical-Flow Thrust-Vectoring of Converging-Diverging Nozzles." Journal of Propulsion and Power 16, no. 2 (2000): 202–6. http://dx.doi.org/10.2514/2.5584.

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8

Niedźwiedzka, Agnieszka. "Numerical modeling of cavitation phenomenon in a two-dimensional converging-diverging nozzle using a homogeneous approach." Mechanik 91, no. 7 (2018): 520–22. http://dx.doi.org/10.17814/mechanik.2018.7.71.

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The article presents results of numerical simulations of cavitation phenomenon in a converging-diverging nozzle using the homogeneous approach. Three cavitation models are considered: the Schnerr and Sauer model, the Singhal et al. model and the Zwart et al. model. The simulations are performed for transient. The geometry is two-dimensional and planar. In the numerical calculations Fluent software was used. The aim of the work is to estimate the possibility of applying of two-dimensional planar numerical simulations of cavitating flows for small-sized converging-diverging nozzles. The motivati

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Krishnamurty, Venkata S., and Wei Shyy. "Effect of Wall Roughness on the Flow Through Converging - Diverging Nozzles." Journal of Propulsion and Power 13, no. 6 (1997): 753–62. http://dx.doi.org/10.2514/2.5248.

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OHIRA, Katsuhide, Tadashi NAKAYAMA, and Takayoshi NAGAI. "Cavitation Flow Instability of Subcooled Liquid Nitrogen in Converging-Diverging Nozzles." TEION KOGAKU (Journal of Cryogenics and Superconductivity Society of Japan) 46, no. 9 (2011): 539–50. http://dx.doi.org/10.2221/jcsj.46.539.

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Dissertations / Theses on the topic "Converging Diverging Nozzles"

1

Fry, Richard N. "Dense gas effects in a converging-diverging nozzle." Thesis, This resource online, 1992. http://scholar.lib.vt.edu/theses/available/etd-12232009-020448/.

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Alkotami, Abdulmalik. "An investigation of cavitation cooling effect in converging-diverging nozzles." Thesis, Kansas State University, 2014. http://hdl.handle.net/2097/32780.

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Master of Science<br>Department of Mechanical and Nuclear Engineering<br>Mohammad H. Hosni<br>A traditional cooling/refrigeration cycle has four main system components which are an evaporator, a compressor, a condenser, and an expansion valve. This type of cycle requires use of refrigerants which have been found to be harmful to the environment, including causing damage to the atmospheric ozone layer. The main objective of the project was to investigate a water-based non-vapor compression cooling system. Water as a working fluid has the advantages of being inexpensive and environmentally safe

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Ilunga, Luc Mwamba. "Performance of a symmetrical converging-diverging tube differential pressure flow meter." Thesis, Cape Peninsula University of Technology, 2014. http://hdl.handle.net/20.500.11838/1029.

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Thesis submitted in fulfilment of the requirements for the degree Master of Technology: Civil Engineering in the Faculty of Engineering at the CAPE PENINSULA UNIVERSITY OF TECHNOLOGY 2014<br>The current problems of orifice, nozzle and Venturi flow meters are that they are limited to turbulent flow and the permanent pressure drop produced in the pipeline. To improve these inadequacies, converging-diverging (C-D) tubes were manufactured, consisting of symmetrical converging and diverging cones, where the throat is the annular section between the two cones, with various angles and diameter ratios

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Murad, Mark Richard. "Radiation View Factors Between A Disk And The Interior Of A Class Of Axisymmetric Bodies Including Converging Diverging Rocket Nozzles." Cleveland State University / OhioLINK, 2008. http://rave.ohiolink.edu/etdc/view?acc_num=csu1210962269.

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Clark, Kylen D. "A Numerical Comparison of Symmetric and Asymmetric Supersonic Wind Tunnels." University of Cincinnati / OhioLINK, 2015. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1447071393.

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Asher, William. "Fluid dynamics of cavitating sonic two-phase flow in a converging-diverging nozzle." Thesis, Kansas State University, 2014. http://hdl.handle.net/2097/17621.

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Master of Science<br>Department of Mechanical and Nuclear Engineering<br>Steven Eckels<br>Both cavitating and flashing flows are important phenomena in fluid flow. Cavitating flow, a common consideration in valves, orifices, and metering devices, is also a concern in loss of coolant accidents for liquid water in power plants when saturation pressures are below atmospheric pressure. Flashing flow is a common consideration for devices such as relief and expansion valves and fluid injectors as well as for loss of coolant accidents in which the coolant’s saturation pressure is above atmospheric.

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Schmidt, Aaron James. "Quantitative measurement and flow visualization of water cavitation in a converging-diverging nozzle." Thesis, Kansas State University, 2016. http://hdl.handle.net/2097/32587.

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Master of Science<br>Department of Mechanical and Nuclear Engineering<br>B. Terry Beck<br>Mohammad H. Hosni<br>Cavitation is the change of a liquid to a two-phase mixture of liquid and vapor, similar to boiling. However, boiling generates a vapor by increasing the liquid temperature while cavitation generates vapor through a decrease in pressure. Both processes are endothermic, removing heat from the surroundings. Both the phase change and heat absorption associated with cavitation provide many engineering applications, including contributing to a new type of refrigeration cycle under devel

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Ahmed, Zayed. "Quantitative flow measurement and visualization of cavitation initiation and cavitating flows in a converging-diverging nozzle." Thesis, Kansas State University, 2017. http://hdl.handle.net/2097/35522.

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Master of Science<br>Department of Mechanical and Nuclear Engineering<br>B. Terry Beck<br>Mohammad H. Hosni<br>Cavitation is the formation of vapor phase from the liquid phase by reduction in its absolute pressure below the saturation pressure. Unlike boiling, where the temperature of the liquid is increased to cause vaporization, the reduction in the pressure alone can cause the liquid to turn into vapor. Cavitation is undesirable in many engineering applications as it is associated with reduction in efficiency and is known to cause damage to pump and propeller components. However, the endoth

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Wang, Peng C. "Large eddy simulation of high speed convergent-divergent nozzle flows." Thesis, Loughborough University, 2013. https://dspace.lboro.ac.uk/2134/11937.

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Interest in developing a detailed understanding of jet plume aerodynamics has increased significantly in recent years, for both civil (noise reduction) and military (Infra-Red signature modelling) aerospace applications. Such flows are critically dependent on turbulence modelling of the jet plume shear layer mixing. Reynolds averaged Navier Stokes (RANS) CFD tends to overpredict while Large Eddy Simulation (LES) CFD underpredicts potential core length. Difficulties in LES begin with the challenge of providing accurate resolution of thin turbulent boundary layers at nozzle exit. Providing physi

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Hlaváček, David. "Kavitující proudění v konvergentně-divergentní trysce." Master's thesis, Vysoké učení technické v Brně. Fakulta strojního inženýrství, 2012. http://www.nusl.cz/ntk/nusl-230045.

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The master´s thesis deals with the flow induced by rotation of cavitating fluid in converging-diverging nozzle, which simulates the vortex rope in impeller of water turbines. Measurement is performed on an experimental circuit in laboratory. Results from experimental measurements are compared with CFD simulation of single and two-phase flow. The main focus is to compare the difference of hydraulic losses and shapes of cavitating structures identified in the experiment and in the simulation.

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Books on the topic "Converging Diverging Nozzles"

1

Carlson, John R. Two-dimensional converging-diverging rippled nozzles at transonic speeds. Langley Research Center, 1994.

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2

Carlson, John R. Two-dimensional converging-diverging rippled nozzles at transonic speeds. National Aeronautics and Space Administration, Langley Research Center, 1994.

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Carlson, John R. Two-dimensional converging-diverging rippled nozzles at transonic speeds. Langley Research Center, 1994.

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4

Landry, John Gary. Nozzle flow with vibrational nonequilibrium. National Aeronautics and Space Administration, 1995.

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Landry, John Gary. Nozzle flow with vibrational nonequilibrium. National Aeronautics and Space Administration, 1995.

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6

G, Taylor John. Internal performance of a hybrid axisymmetric/nonaxisymmetric convergent-divergent nozzle. Langley Research Center, 1991.

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7

Hamed, A. High speed nozzles task: Final report. University of Cincinnati, 1995.

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8

Foley, Robert J. Static thrust-vectoring performance of nonaxisymmetric convergent-divergent nozzles with post-exit yaw vanes. Langley Research Center, 1991.

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9

Asbury, Scott C. Effects of internal yaw-vectoring devices on the static performance of a pitch-vectoring nonaxisymmetric convergent-divergent nozzle. Langley Research Center, 1993.

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10

G, Taylor John. Static investigation of a two-dimensional convergent-divergent exhaust nozzle with multiaxis thrust-vectoring capability. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

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Book chapters on the topic "Converging Diverging Nozzles"

1

Hasini, Hasril, Norhazwani Abd Malek, and Mohd Zamri Yusoff. "Numerical Modelling of Dry and Wet Steam Flows in Converging-Diverging Nozzles." In The Malaysia-Japan Model on Technology Partnership. Springer Japan, 2014. http://dx.doi.org/10.1007/978-4-431-54439-5_10.

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Das, Buddha Dev, Rajdeep Sardar, Sandip Sarkar, and Nirmal Kumar Manna. "Compressible Flow Through Convergent–Divergent Nozzle." In Lecture Notes in Mechanical Engineering. Springer Singapore, 2021. http://dx.doi.org/10.1007/978-981-33-4165-4_32.

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Miyazato, Y., T. Aoki, N. Kondoh, et al. "Experimental investigation on supersonic jet noise from convergent-divergent nozzles." In Shock Waves. Springer Berlin Heidelberg, 2005. http://dx.doi.org/10.1007/978-3-540-27009-6_203.

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Opalka, Klaus-Otto. "Optical Studies of the Flow Start-up in Convergent-Divergent Nozzles." In Shock Waves @ Marseille I. Springer Berlin Heidelberg, 1995. http://dx.doi.org/10.1007/978-3-642-78829-1_49.

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Park, Sung Han, J. W. Han, Chang Hee Lee, and Hyung Jun Kim. "Effect of Curvature on Gas-Particle Flow in Converging and Diverging Supersonic Nozzle." In Solid State Phenomena. Trans Tech Publications Ltd., 2007. http://dx.doi.org/10.4028/3-908451-31-0.1697.

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Prabhu, L., N. Kiran Jadediya, P. Gangadhar Venkata Ramana, and J. Srinivas. "Numerical Investigation on Optimized Convergent Divergent Nozzle in 3S Separator Device." In Lecture Notes in Mechanical Engineering. Springer Singapore, 2020. http://dx.doi.org/10.1007/978-981-15-6619-6_10.

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Petruccelli, Giuseppe, Antti Uusitalo, Aki Grönman, Teemu Turunen-Saaresti, and Marta Zocca. "Design of a Closed-Loop Supercritical Carbon Dioxide Wind Tunnel: Numerical Modelling of Non-equilibrium Condensation in a Converging-Diverging Nozzle." In Proceedings of the 3rd International Seminar on Non-Ideal Compressible Fluid Dynamics for Propulsion and Power. Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-69306-0_11.

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"Variable Convergent-Divergent Exhaust Nozzle Aerodynamics." In Aircraft Propulsion Systems Technology and Design. American Institute of Aeronautics and Astronautics, 1989. http://dx.doi.org/10.2514/5.9781600861499.0299.0336.

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"Compressible Gas Dynamics: Design of a Converging-Diverging Nozzle." In Applying Engineering Thermodynamics. WORLD SCIENTIFIC, 2021. http://dx.doi.org/10.1142/9789811205248_0024.

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"Numerical Investigation of Cavitation-Regimes in a Converging-Diverging Nozzle." In Proceedings of the 10th International Symposium on Cavitation (CAV2018). ASME Press, 2018. http://dx.doi.org/10.1115/1.861851_ch145.

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Conference papers on the topic "Converging Diverging Nozzles"

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Li, Ding, Guoping Xia, and Charles Merkle. "Analysis of Real Fluid Flows in Converging Diverging Nozzles." In 33rd AIAA Fluid Dynamics Conference and Exhibit. American Institute of Aeronautics and Astronautics, 2003. http://dx.doi.org/10.2514/6.2003-4132.

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Rafael Dias Barreto and Felipe Bastos de Freitas Rachid. "ONE-DIMENSIONAL GASEOUS CAVITATING FLOWS IN CONVERGING-DIVERGING NOZZLES." In 23rd ABCM International Congress of Mechanical Engineering. ABCM Brazilian Society of Mechanical Sciences and Engineering, 2015. http://dx.doi.org/10.20906/cps/cob-2015-0724.

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Ping, Zhu, Liya Hou, and Weiyi Zhang. "The Measurement on Micro-Jet Impulse Based on Laser Interferometer." In ASME 2009 Fluids Engineering Division Summer Meeting. ASMEDC, 2009. http://dx.doi.org/10.1115/fedsm2009-78030.

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In the paper the heterodyne laser vibrometer combined with torsion pendulum system is employed to measure contactless the oscillating velocity of the horizontal target struck by pulse hydrone micro-jet in the experimental platform, which has the feature of measuring precisely impulse (measurement error ≤ 0.618%). The oscillating velocities of pulse micro-jet from converging-diverging, converging and cylindrical nozzles striking on horizontal target are measured respectively in normal atmosphere, and the values of the impulses are calculated by employing the dynamic character equation of force

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Tyagi, Manav, and Raman Sujith. "Nonlinear Distortion of Finite Amplitude Waves Propagating in Converging-Diverging Nozzles." In 42nd AIAA Aerospace Sciences Meeting and Exhibit. American Institute of Aeronautics and Astronautics, 2004. http://dx.doi.org/10.2514/6.2004-1130.

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Krishnamurty, Venkata, Wei Shyy, Siddharth Thakur, Venkata Krishnamurty, Wei Shyy, and Siddharth Thakur. "Effect of wall roughness on the flow through converging-diverging nozzles." In 35th Aerospace Sciences Meeting and Exhibit. American Institute of Aeronautics and Astronautics, 1997. http://dx.doi.org/10.2514/6.1997-208.

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Kim, Sangwon, Charles Mitchell, and Allan Kirkpatrick. "Design and Evaluation of High Pressure Fuel Valve Nozzles Using the Method of Characteristics and CFD." In ASME 2003 Internal Combustion Engine and Rail Transportation Divisions Fall Technical Conference. ASMEDC, 2003. http://dx.doi.org/10.1115/icef2003-0742.

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The topic of this paper is the design of fuel valve nozzles for natural gas engines that maximize the kinetic energy and momentum of the injected fuel and maintain a required mass flow rate. The nozzle design used both the method of characteristics and computational fluid dynamics (CFD). Three types of nozzles were designed: a converging-diverging nozzle, three conical nozzles and an aerospike nozzle. The evaluation of the performance of the nozzle designs was conducted using Computational Fluid Dynamics. CFD simulations were used to calculate the average axial momentum per unit fuel mass and

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Yazdani, Miad, Thomas D. Radcliff, Abbas A. Alahyari, and Mohsen Farzad. "Numerical Modeling and Validation of Supersonic Two-Phase Flow of CO2 in Converging-Diverging Nozzles." In ASME 2011 International Mechanical Engineering Congress and Exposition. ASMEDC, 2011. http://dx.doi.org/10.1115/imece2011-64783.

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CO2 is an attractive alternative to conventional refrigerants due to its low direct global warming effects. Unfortunately, CO2 and many alternative refrigerants have lower thermodynamic performance resulting in larger indirect emissions. Effective use of ejectors to recover part of the lost expansion work, which occurs in throttling devices can close this performance gap and enable the use of CO2. In an ejector, the pressure of the motive fluid is converted into momentum through a choked converging-diverging nozzle, which then entrains and raises the energy of a lower-momentum suction flow. In

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ZHA, GE-CHENG, and E. BILGEN. "Effect of throat contouring on two-dimensional converging-diverging nozzles using URS method." In 10th Applied Aerodynamics Conference. American Institute of Aeronautics and Astronautics, 1992. http://dx.doi.org/10.2514/6.1992-2659.

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Mohd Hafiz Mohd Noh, Ahmad Hussein Abdul Hamid, Rahim Atan, and Helmi Rashid. "Numerical investigation of chocked converging-diverging nozzles for thruster application (normal shock wave)." In 2010 International Conference on Science and Social Research (CSSR). IEEE, 2010. http://dx.doi.org/10.1109/cssr.2010.5773722.

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Choudhary, Kapil Dev, Shyam Sunder Yadav, and Mani Sankar Dasgupta. "CLASSICAL NUCLEATION THEORY BASED SIMULATIONS OF NON-EQUILIBRIUM CONDENSATION OF CARBON DIOXIDE INSIDE CONVERGING-DIVERGING NOZZLES." In 5-6th Thermal and Fluids Engineering Conference (TFEC). Begellhouse, 2021. http://dx.doi.org/10.1615/tfec2021.cnd.036103.

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Reports on the topic "Converging Diverging Nozzles"

1

L. E. Thode, M. C. Cline, B. G. DeVolder, M. S. Sahota, and D. K. Zerkle. Comparison among five hydrodynamic codes with a diverging-converging nozzle experiment. Office of Scientific and Technical Information (OSTI), 1999. http://dx.doi.org/10.2172/752367.

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