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Relevant bibliographies by topics / Blunt body

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Academic literature on the topic 'Blunt body'

Author: Grafiati

Published: 6 September 2023

Last updated: 26 July 2025

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Journal articles on the topic "Blunt body"

1

Patel, Payal, Riddhi Patel, Payal Rathod, Nikita Prajapati, Nizama Vishal, and Rana Mehul. "Analysis of Drag Reduction over Different Types of Blunt Bodies at Different Angle of Attack." International Journal of Innovative Science and Research Technology 8, no. 3 (2023): 797–805. https://doi.org/10.5281/zenodo.7767592.

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The main intention of this project is to do relative analysis of Drag Reduction over Blunt Bodies at varied Angles of Attack in Supersonic Flow. In this project we have taken plain blunt body attached with different types of spikes which are like as 1. Blunt nose 2. Conical spike 3. Flat faced aero disc 4. Hemispherical spike 5. Breathing Blunt nose. For competitive analysis and results based on the different angle of attack with 0, 5 and 8 on that blunt body with spikes. Numerical simulation was carried out using CFD with SST komega model adopted. The hemispherical body is found to be efficie

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Fan, Liguo, Guoqiang Liu, Xianjin Song, Ce Xiang, Jiacheng Wei, and Hui Xia. "Simulation and Experiments on Optimization of Vortex-Induced Vibration Power Generation System Based on Side-by-Side Double Blunt Bodies." Energies 17, no. 21 (2024): 5291. http://dx.doi.org/10.3390/en17215291.

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In order to improve the utilization efficiency of converting low-flow current energy into electric energy for Reynolds number 10,000 ≤ Re ≤ 40,000, this paper proposes a vortex-induced vibration power generation system based on a side-by-side double blunt body. In this system, the side-by-side double blunt body structure is used in the current energy capture part to enhance the collection of low-flow current energy; the permanent magnet linear motor is used in the electric energy conversion part to improve the efficiency of electric energy conversion; and a laboratory device is constructed for

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3

Li, Yong Hong, Xin Wu Tang, and Wei Qun Zhou. "Aerodynamic and Numerical Study on the Influence of Spike Shapes at Mach 1.5." Advanced Materials Research 1046 (October 2014): 177–81. http://dx.doi.org/10.4028/www.scientific.net/amr.1046.177.

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Taking into account the issue of configuration or aerodynamic heating, most supersonic and hypersonic flight vehicles have to use the blunt-nosed body. However, in supersonic especially in hypersonic flow the strong bow shock ahead of the blunt nose introduces a rather high shock drag that affects the aerodynamic performance of the vehicles seriously. A spike mounted on a blunt body during its flight pushes the strong bow shock away from the body surface and forms recirculation flow with low pressure ahead of the body surface, and then decreases the drag. The drag reduction effects of spikes i

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4

Hollis, Brian R., and Salvatore Borrelli. "Aerothermodynamics of blunt body entry vehicles." Progress in Aerospace Sciences 48-49 (January 2012): 42–56. http://dx.doi.org/10.1016/j.paerosci.2011.09.005.

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Watanabe, Yasumasa, Kojiro Suzuki, and Ethirajan Rathakrishnan. "Aerodynamic characteristics of breathing blunt nose configuration at hypersonic speeds." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 231, no. 5 (2016): 840–58. http://dx.doi.org/10.1177/0954410016643979.

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Breathing blunt nose technique is one of the promising methods for reducing the drag of blunt-nosed body at hypersonic speeds. The air, traversed by the bow shock positioned ahead of the nose, at the stagnation region is allowed to enter through a hole at the blunt-nose and ejected at the rear part (base region) of the body. This manipulation reduces the positive pressure over the stagnation regions of the nose and increases the pressure at the base, resulting in reduced suction at the base. The simultaneous manifestation of reducing the compression at the nose and suction at the base regions

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Rofi’i, Ahmad Syafiq, Aditia Aulia, Muhammad Ferry Fadri, Muhammad Haidar Syarif, Elvira Rosmawati Rahman, and Gunawan Dwi Haryadi. "Numerical investigation on the effect of blunt body deflector on darieus turbine performance." E3S Web of Conferences 475 (2024): 03002. http://dx.doi.org/10.1051/e3sconf/202447503002.

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One of the renewable energy source that is abundant but has not been used optimally is wind energy. Roads are currently the main transportation infrastructure along with the increasing number of motorized vehicles. Wind is one of the best renewable energy sources that can be utilized on the highway where it can be used as a power source to drive the Vertical Axis Wind Turbine (VAWT). Darrieus type turbines can operate at low wind speeds and do not require a specific wind direction. However, the installation of this wind turbine on the highway can be hampered due to the presence of highway ligh

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Kazemba, Cole D., Robert D. Braun, Ian G. Clark, and Mark Schoenenberger. "Survey of Blunt-Body Supersonic Dynamic Stability." Journal of Spacecraft and Rockets 54, no. 1 (2017): 109–27. http://dx.doi.org/10.2514/1.a33552.

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Shang, J. S., J. Hayes, J. Menart, and J. Miller. "Blunt Body in Hypersonic Electromagnetic Flow Field." Journal of Aircraft 40, no. 2 (2003): 314–22. http://dx.doi.org/10.2514/2.3095.

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Carlson, Henry A. "Aerothermodynamic Analyses of Hypersonic, Blunt-Body Flows." Journal of Spacecraft and Rockets 36, no. 6 (1999): 912–15. http://dx.doi.org/10.2514/2.3511.

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Knops, R. J., and Piero Villaggio. "An Approximate Treatment of Blunt Body Impact." Journal of Elasticity 72, no. 1-3 (2003): 213–28. http://dx.doi.org/10.1023/b:elas.0000018776.92471.36.

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Dissertations / Theses on the topic "Blunt body"

1

Dominy, Robert Gerald. "Rarefied hypersonic shock wave and blunt body flows." Thesis, Imperial College London, 1988. http://hdl.handle.net/10044/1/47034.

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Castledine, Andre J. "Investigation of the fluid flow around blunt body samplers." Thesis, University of Leeds, 1992. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.305756.

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Ess, Peter. "Numerical simulation of blunt body-generated detonation wave ramjet flowfields." Thesis, National Library of Canada = Bibliothèque nationale du Canada, 1999. http://www.collectionscanada.ca/obj/s4/f2/dsk1/tape8/PQDD_0019/MQ45873.pdf.

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Jain, Sunny. "Hypersonic nonequilibrium flow simulations over a blunt body using bgk simulations." [College Station, Tex. : Texas A&M University, 2007. http://hdl.handle.net/1969.1/ETD-TAMU-2406.

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Ess, Peter. "Numerical simulation of blunt-body generated detonation waves in viscous hypersonic ducted flows." Thesis, University of Bristol, 2003. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.288263.

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Johnson, Joshua E. "Multidisciplinary optimization of non-spherical, blunt-body heat shields for a planetary entry vehicle." College Park, Md. : University of Maryland, 2006. http://hdl.handle.net/1903/3766.

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Thesis (M.S.) -- University of Maryland, College Park, 2006.<br>Thesis research directed by: Dept. of Aerospace Engineering. Title from t.p. of PDF. Includes bibliographical references. Published by UMI Dissertation Services, Ann Arbor, Mich. Also available in paper.

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Johnson, Joshua E. "Aerothermodynamic optimization of earth entry blunt body heat shields for lunar and Mars return." College Park, Md.: University of Maryland, 2009. http://hdl.handle.net/1903/9177.

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Thesis (Ph.D.) -- University of Maryland, College Park, 2009.<br>Thesis research directed by: Dept. of Aerospace Engineering. Title from t.p. of PDF. Includes bibliographical references. Published by UMI Dissertation Services, Ann Arbor, Mich. Also available in paper.

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Aubuchon, Vanessa V. "Damping Effects of Drogue Parachutes on Orion Crew Module Dynamics." Thesis, Virginia Tech, 2013. http://hdl.handle.net/10919/23327.

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Currently, simulation predictions of the Orion Crew Module (CM) dynamics with drogue parachutes deployed are under-predicting the amount of damping as seen in free-flight tests. The Apollo Legacy Chute Damping model has been resurrected and applied to the Orion system. The legacy model has been applied to predict CM damping under drogue parachutes for both Vertical Spin Tunnel free flights and the Pad Abort-1 flight test. Comparisons between the legacy Apollo prediction method and test data are favorable. A key hypothesis in the Apollo legacy drogue damping analysis is that the drogue para

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Kurits, Inna. "Quantitative global heat-transfer measurements using temperaure-sensitive [sic] paint on a blunt body in hypersonic flows." College Park, Md. : University of Maryland, 2008. http://hdl.handle.net/1903/8302.

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Thesis (M.S.) -- University of Maryland, College Park, 2008.<br>Thesis research directed by: Dept. of Aerospace Engineering. Title from t.p. of PDF. Includes bibliographical references. Published by UMI Dissertation Services, Ann Arbor, Mich. Also available in paper.

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Pinn, Jarred Michael. "Effect of End-Plate Tabs on Drag Reduction of a 3D Bluff Body with a Blunt Base." DigitalCommons@CalPoly, 2012. https://digitalcommons.calpoly.edu/theses/698.

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This thesis involves the experimental testing of a bluff body with a blunt base to evaluate the effectiveness of end-plate tabs in reducing drag. The bluff body is fitted with interchangeable end plates; one plate is flush with the rest of the exterior and the other plate has small tabs protruding perpendicularly into the flow. The body is tested in the Cal Poly 3ft x 4ft low speed wind tunnel. Testing is conducted in three phases. The first phase was the hot-wire measurement of streamwise velocity of the near wake behind the bluff body. An IFA300 thermal anemometry system with a hot-wire prob

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Books on the topic "Blunt body"

1

Dunnett, Sarah Jane, and Derek Binns Ingham. The Mathematics of Blunt Body Sampling. Springer Berlin Heidelberg, 1988. http://dx.doi.org/10.1007/978-3-642-83563-6.

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Dunnett, S. J. The mathematics of blunt body sampling. Springer-Verlag, 1988.

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3

L, Montagne J., and Ames Research Center, eds. Hypersonic blunt body computations including real gas effects. National Aeronautics and Space Administration, Ames Research Center, 1988.

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4

K, Dogra V., and United States. National Aeronautics and Space Administration., eds. Effects of chemistry on blunt-body wake structure. American Institute of Aeronautics and Astronautics, 1995.

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5

Institute for Computer Applications in Science and Engineering., ed. Spectral solution of the viscous blunt body problem. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1994.

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6

K, Dogra V., and United States. National Aeronautics and Space Administration., eds. Effects of chemistry on blunt-body wake structure. American Institute of Aeronautics and Astronautics, 1995.

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L, Montagne J., and Ames Research Center, eds. Hypersonic blunt body computations including real gas effects. National Aeronautics and Space Administration, Ames Research Center, 1988.

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8

Ess, Peter. Numerical simulation of blunt body generated detonation wave ramjet flowfields. National Library of Canada, 1999.

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9

M, Price J., and United States. National Aeronautics and Space Administration., eds. Review of blunt body wake flows at hypersonic low density conditions. American Institute of Aeronautics and Astronautics, 1996.

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10

Kopriva, David A. Spectral solution of the viscous blunt body problem. II: Multidomain approximation. Langley Research Center, 1994.

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Book chapters on the topic "Blunt body"

1

Mölder, Sannu. "Blunt Body Flow — The Transonic Region." In Shock Waves @ Marseille I. Springer Berlin Heidelberg, 1995. http://dx.doi.org/10.1007/978-3-642-78829-1_15.

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2

Schall, E., and D. Zeitoun. "Nonequilibrium Hypersonic Flow Around a Blunt Body." In Shock Waves @ Marseille II. Springer Berlin Heidelberg, 1995. http://dx.doi.org/10.1007/978-3-642-78832-1_53.

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3

Shen, Junwei, Shaowu Ma, Yuning Zhang, and Jian Chang. "Visualization Research on Blunt Body Wake Dynamics." In SpringerBriefs in Energy. Springer Nature Switzerland, 2025. https://doi.org/10.1007/978-3-031-82754-9_5.

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4

Montagné, J. L., H. C. Yee, G. H. Klopfer, and M. Vinokur. "Hypersonic Blunt Body Computations Including Real Gas Effects." In Nonlinear Hyperbolic Equations — Theory, Computation Methods, and Applications. Vieweg+Teubner Verlag, 1989. http://dx.doi.org/10.1007/978-3-322-87869-4_42.

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5

Fey, Michael, Rolf Jeltsch, and Peter Karmann. "Special aspects of reacting inviscid blunt body flow." In Hypersonic Flows for Reentry Problems. Springer Berlin Heidelberg, 1992. http://dx.doi.org/10.1007/978-3-642-77922-0_55.

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6

Délery, Jean. "Separation Induced by an Obstacle or a Blunt Body." In Three-dimensional Separated Flow Topology. John Wiley & Sons, Inc., 2013. http://dx.doi.org/10.1002/9781118578544.ch5.

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7

Reshotko, Eli, and Anatoli Tumin. "The Blunt Body Paradox — A Case for Transient Growth." In Laminar-Turbulent Transition. Springer Berlin Heidelberg, 2000. http://dx.doi.org/10.1007/978-3-662-03997-7_60.

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Harris, Anne F. "Hewn." In Inhuman Nature. punctum books, 2014. https://doi.org/10.21983/p3.0078.1.04.

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Hewn is a status in the ecology of the inhuman, a state of being that is as old as human presence outside of Eden. Its ancient word of origin, "hew," carries an onomatopoeic trace of the effort of cutting down, the blunt force seized by the body to bring down the thing.

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Shi, Jiatong, Ketian Shi, and Liang Zhang. "Uniform Aero-Heating Flux Design for a Hypersonic Blunt Body." In Lecture Notes in Electrical Engineering. Springer Singapore, 2019. http://dx.doi.org/10.1007/978-981-13-3305-7_27.

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Ohnishi, N., Y. Inabe, K. Ozawa, and K. Ohtani. "Critical Condition of Bow-Shock Instability Around Edged Blunt Body." In 31st International Symposium on Shock Waves 2. Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-319-91017-8_135.

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Conference papers on the topic "Blunt body"

1

PEERY, K., and S. IMLAY. "Blunt-body flow simulations." In 24th Joint Propulsion Conference. American Institute of Aeronautics and Astronautics, 1988. http://dx.doi.org/10.2514/6.1988-2904.

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Vaganov, A. V., A. Yu Noev, V. N. Radchenko, and A. G. Zdor. "INVESTIGATION OF BLUNT-BODY PARADOX." In INTERNATIONAL CONFERENCE ON THE METHODS OF AEROPHYSICAL RESEARCH. Издательство Сибирского отделения РАН, 2022. http://dx.doi.org/10.53954/9785604788974_165.

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PEERY, K., S. IMLAY, and J. KATSANDRES. "Real-gas blunt-body flow simulations." In 23rd Joint Propulsion Conference. American Institute of Aeronautics and Astronautics, 1987. http://dx.doi.org/10.2514/6.1987-2179.

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Shang, J., J. Hayes, J. Miller, and J. Menart. "Blunt body in hypersonic electromagnetic flow field." In 32nd AIAA Plasmadynamics and Lasers Conference. American Institute of Aeronautics and Astronautics, 2001. http://dx.doi.org/10.2514/6.2001-2803.

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Oliveira, Maria, and Chaoqun Liu. "Implicit LES for Shock/Blunt Body Interaction." In 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. American Institute of Aeronautics and Astronautics, 2010. http://dx.doi.org/10.2514/6.2010-874.

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Poggie, J., and D. Gaitonde. "Magnetic control of hypersonic blunt body flow." In 38th Aerospace Sciences Meeting and Exhibit. American Institute of Aeronautics and Astronautics, 2000. http://dx.doi.org/10.2514/6.2000-452.

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Dwivedi, Anubhav, and Mihailo R. Jovanovic. "Noise amplification in hypersonic blunt body flows." In AIAA AVIATION 2023 Forum. American Institute of Aeronautics and Astronautics, 2023. http://dx.doi.org/10.2514/6.2023-3709.

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STALKER, R. "A similarity transformation for blunt body flows." In 24th Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics, 1986. http://dx.doi.org/10.2514/6.1986-125.

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Rosema, Christopher, and David Riddle. "Aerodynamic Assessment of Several Blunt Body Configurations." In 47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition. American Institute of Aeronautics and Astronautics, 2009. http://dx.doi.org/10.2514/6.2009-910.

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Alhussan, Khaled. "Multi-Fins Decelerator for Blunt Body in Turbulent Flows." In ASME/JSME 2007 5th Joint Fluids Engineering Conference. ASMEDC, 2007. http://dx.doi.org/10.1115/fedsm2007-37460.

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The aim of this research is to use the numerical analysis techniques to design deceleration devices for a blunt body. In this paper a qualitative analysis of the flow structure over a blunt body with and without multi-fins decelerator was shown. In some applications of aerodynamics, a deceleration of a moving body is required therefore the prediction and controlling of the drag is essential. The deceleration devices such as air bag or fins can be added to the body to increase the aerodynamics drag. For a supersonic speed, a flow around blunt body is complicated due to the detached shock wave,

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Reports on the topic "Blunt body"

1

Candler, Graham V. Effect of Internal Energy Excitation on Supersonic Blunt-Body Aerodynamics. Defense Technical Information Center, 2001. http://dx.doi.org/10.21236/ada387503.

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Taylor, Paul A., and Candice Frances Cooper. Simulation of Blast and Behind-Armor Blunt Trauma to Life-Critical Organs in the Human Body. Office of Scientific and Technical Information (OSTI), 2016. http://dx.doi.org/10.2172/1562207.

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