Relevant bibliographies by topics / Subsonic

Academic literature on the topic 'Subsonic'

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Published: 4 June 2021
Last updated: 12 February 2022

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Journal articles on the topic "Subsonic"

1

Heins, Paul, and S. Perkins. "Subsonic Booms." Science News 164, no. 18 (November 1, 2003): 287. http://dx.doi.org/10.2307/4018958.

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Zhu, Wen-Xiang, and Wei Liu. "Magnetic snakes subsonic." AME Medical Journal 5 (December 2020): 44. http://dx.doi.org/10.21037/amj.2020.03.01.

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Salo, Janne, and Martti M. Salomaa. "Subsonic nondiffracting waves." Acoustics Research Letters Online 2, no. 1 (January 2001): 31–36. http://dx.doi.org/10.1121/1.1350398.

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Loseva, T. V., and I. V. Nemchinov. "Subsonic radiation waves." Fluid Dynamics 28, no. 5 (1994): 720–33. http://dx.doi.org/10.1007/bf01050059.

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Xie, Chunjing, and Zhouping Xin. "Global subsonic and subsonic-sonic flows through infinitely long nozzles." Indiana University Mathematics Journal 56, no. 6 (2007): 2991–3024. http://dx.doi.org/10.1512/iumj.2007.56.3108.

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Florin, MUNTEANU, OPREAN Corneliu, and STOICA Corneliu. "INCAS SUBSONIC WIND TUNNEL." INCAS BULLETIN 1, no. 1 (September 24, 2009): 12–14. http://dx.doi.org/10.13111/2066-8201.2009.1.1.3.

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Somers, D. M. "Subsonic aerofoil design 2010." Aeronautical Journal 115, no. 1165 (March 2011): 137–46. http://dx.doi.org/10.1017/s0001924000005546.

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Abstract The state of the art as practiced by a handful of aerofoil designers is discussed. The methods used, both theoretical and experimental, are described. Aerofoil/application design integration and expansion of the design envelope to lower and higher Reynolds numbers are illustrated by examples, including the slotted, natural-laminar-flow aerofoil.
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Moosavi, M. R., A. R. Naddaf Oskouei, and A. Khelil. "Flutter of subsonic wing." Thin-Walled Structures 43, no. 4 (April 2005): 617–27. http://dx.doi.org/10.1016/j.tws.2004.10.001.

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Cheng, Jianfeng, and Lili Du. "Compressible Subsonic Impinging Flows." Archive for Rational Mechanics and Analysis 230, no. 2 (May 15, 2018): 427–58. http://dx.doi.org/10.1007/s00205-018-1249-x.

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Xie, Chunjing, and Zhouping Xin. "Global subsonic and subsonic-sonic flows through infinitely long axially symmetric nozzles." Journal of Differential Equations 248, no. 11 (June 2010): 2657–83. http://dx.doi.org/10.1016/j.jde.2010.02.007.

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Dissertations / Theses on the topic "Subsonic"

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Ho, S. S. H. "Subsonic intake duct flows." Thesis, University of Salford, 1990. http://usir.salford.ac.uk/2213/.

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Here both S-shaped and singly curved (here classified as S-shaped) duct diffusers for intakes in aeronautical propulsion systems are studied. The results are applicable in other situations where similar ducts occur; for example on V/STOL aircraft employing re-direction of thrust, intercomponent ducting in high bypass ratio engines, etc. An open circuit static test rig, capable of mass flow rates of 5 kg/s, and three-dimensional instrumentation were established. Flow measurements were made in S-shaped intake duct diffusers for rear mounted gas turbine engines in both aircraft and air-breathing missiles. These designs are intended for ventral type inlet installation. These ducts possess cross-sectional shape transitions, from oblate to circular, with area increase and annular ducts at the engine face. The work was aimed at both fundamental understanding of the flows and at establishing test data for the prediction methods. Tests were performed at throat Mach numbers of nominally 0.15 and 0.6 and in the unit Reynolds number range of 3x10_6/m - 2x10_7/m for three different ducts each having different upstream bends but common downstream bends. Detailed boundary layer surveys were made to establish plane of symmetry growth of the viscous region and the extent of three-dimensionality away from the plane of symmetry. Data are presented in the form of velocity profiles, streamwise and cross-flow, integral thicknesses and surface pressure fields. Engine face distortion is assessed from full outlet flow surveys. Flow visualization was recorded using surface oil flow techniques. Evidence is presented of a trend towards three-dimensional separation as the upstream bend increases in severity. For the most extreme case large regions of complex three-dimensional separated flow occur and topological analysis of the recorded surface oil flow pattern allows reconstruction of the separating flow. Clear correlations are established between flow visualization results and flow measurements yielding better understanding. Finally, results were compared with a three-dimensional compressible prediction method.
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Ho, Y. K. "Supersonic and subsonic radial jets." Thesis, University of Manchester, 1987. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.378306.

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Tambe, Samir B. "Liquid Jets in Subsonic Crossflow." University of Cincinnati / OhioLINK, 2004. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1100876702.

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Weil, Samuel P. "Subsonic Performance of Ejector Systems." University of Cincinnati / OhioLINK, 2015. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1428048770.

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Su, Wei-Jen Dimotakis Paul E. Dimotakis Paul E. "Aerodynamic control for a subsonic diffuser /." Diss., Pasadena, Calif. : California Institute of Technology, 2001. http://resolver.caltech.edu/CaltechETD:etd-09042007-145002.

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Kakkavas, Constantinos. "Computational investigation of subsonic torsional airfoil flutter." Thesis, Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 1998. http://handle.dtic.mil/100.2/ADA359731.

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Thesis (M.S. in Aeronautical Engineering) Naval Postgraduate School, December 1998.
"December 1998." Thesis advisor(s): Max F. Platzer, Kevin D. Jones. Includes bibliographical references (p. 89-90). Also available online.
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Murray, Nathan E. "Flow field dynamics in subsonic cavity flows /." Full text available from ProQuest UM Digital Dissertations, 2006. http://0-proquest.umi.com.umiss.lib.olemiss.edu/pqdweb?index=0&did=1299816381&SrchMode=1&sid=4&Fmt=2&VInst=PROD&VType=PQD&RQT=309&VName=PQD&TS=1193667418&clientId=22256.

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Lawrence, Jack. "Aeroacoustic interactions of installed subsonic round jets." Thesis, University of Southampton, 2014. https://eprints.soton.ac.uk/367059/.

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Additional noise sources are generated when an aircraft engine is mounted beneath a wing. The two main installation sources include: (1) reflection of the exhaust jet mixing noise from the underside of the wing, and (2) interaction between the turbulent jet plume and the trailing edge of the wing, or deployed flap. The strength, directivity and frequency content of these particular sources all serve to increase the time-averaged flyover aircraft noise level heard on the ground by residents beneath the flight path. As the bypass ratio and nacelle diameter of modern turbofan engines continues to increase, constraints on ground clearance are forcing under-wing-mounted engines to be coupled more closely to the wing and flap system, which, in turn, serves to accentuate both of these noise sources. Close-coupled nacelle-airframe designs are now a critical issue surrounding efforts to meet the future environmental targets for quieter civil aircraft. This research is principally aimed at understanding and predicting the groundpropagating noise generated by the latter of these two installed jet noise sources. In order to characterise the jet-surface interaction noise source, however, it is first necessary to isolate it. A small 1/50th model-scale acoustic experiment, therefore, is conducted in a semi-anechoic university laboratory using a single stream jet installed beneath a flat plate. Both far-field acoustic and near-field plate surface pressure data are measured to investigate the jet-surface interaction noise source. Results from this fundamental experiment are then used to help drive a larger, and more realistic, 1/10th modelscale test campaign, at QinetiQ's Noise Test Facility, where 3D wing geometry effects, Reynolds number scaling effects and static-to-flight effects are investigated. A jet-flap impingement tonal noise phenomenon is also identified and investigated at particularly closely-coupled jet-wing configurations. Finally, the first version of a fast, semi-empirical engineering tool is developed to predict the additional noise caused by jet-wing interaction noise, under static ambient flow conditions. It is hoped that this tool will serve to inform future commercial aircraft design decisions and, thus, will help to protect the acoustic environment of residents living beneath flight paths.
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Sheen, Shaw-Ching. "Large eddy simulation of subsonic mixing layers." Diss., Virginia Tech, 1993. http://hdl.handle.net/10919/40183.

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Kim, Meung Jung. "Application of panel methods for subsonic aerodynamics." Diss., Virginia Polytechnic Institute and State University, 1985. http://hdl.handle.net/10919/52299.

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Several panel methods are developed to model subsonic aerodynamics. The vorticity panel method for two-dimensional problems is capable of handling general unsteady, potential, lifting flows. The lifting surface is modelled with a vortex sheet and the wakes by discrete vortices. As an imitation of the conditions at the trailing edge, stagnation conditions on both surfaces are used. The over-determined system is solved by an optimization scheme. The present predictions are in good agreement with experimental data and other computations. Moreover the present approach provides an attractive alternative to those developed earlier. Two panel methods for three-dimensional nonlifting problems are developed. One uses source distributions over curved elements and the other vorticity distributions over flat elements. For the source formulation, the effect of weakly nonlinear geometry on the numerical results is shown to accelerate the convergence of numerical values in general. In addition, the extensive comparisons between two formulations reveal that the voticity panel method is even more stable and accurate than the curved source panel method. Another vorticity panel method is developed to study the lifting l flows past three-dimensional bodies with sharp edges. The body is modelled by single vortex sheet for thin bodies and two vortex sheets for thick bodies while the wakes are modelled with a number of strings of discrete vortices. The flows are assumed to separate along the the sharp edges. The combination of continuous vorticity on the lifting surface and discrete vortices in the wakes yields excellent versatility and the capability of handling the tightly rolled wakes and predicting continuous pressure distributions on the lifting surface. The method is applied to thin and thick low-aspect-ratio delta wings and rectangular wings. The computed aerodynamic forces and wake shapes are in quantitative agreement with experimental data and other computational results.
Ph. D.
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Books on the topic "Subsonic"

1

Subsonic airplane performance. Warrendale, PA: Society of Automotive Engineers, 1994.

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2

Ho, Sidney Shiu Hin. Subsonic intake duct flows. Salford: University of Salford, 1990.

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Ingenito, Antonella. Subsonic Combustion Ramjet Design. Cham: Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-66881-5.

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Goldstein, Marvin E. Aeroacoustics of subsonic turbulent shear flows. [Washington, DC]: National Aeronautics and Space Administration, 1987.

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5

Isaacs, D. Store carriage loads at subsonic speeds. London: HMSO, 1988.

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Gentry, Garl L. The Langley 14- by 22-foot subsonic tunnel: description, flow characteristics, and guide for users. Hampton, Va: Langley Research Center, 1990.

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Bowcutt, K. G. The use of panel methods for the development of low subsonic wall interference and blockage corrections. New York: AIAA, 1985.

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Rudolph, Peter K. C. High-lift systems on commercial subsonic airliners. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1996.

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Nagabushana, K. A. Heat transfer from cylinders in subsonic slip flows. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

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Snyder, Aaron. Numerical simulation of subsonic and transonic propeller flow. [Washington, DC]: National Aeronautics and Space Administration, 1988.

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Book chapters on the topic "Subsonic"

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Weik, Martin H. "subsonic." In Computer Science and Communications Dictionary, 1684. Boston, MA: Springer US, 2000. http://dx.doi.org/10.1007/1-4020-0613-6_18504.

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Self, Douglas. "Subsonic Filtering." In Electronics for Vinyl, 201–52. New York ; London : Routledge, 2017.: Routledge, 2017. http://dx.doi.org/10.4324/9781315202174-12.

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Makarenko, T. M., T. U. Volnova, T. N. Bezmenova, and V. I. Ribakov. "Subsonic Jet Visualization." In Flow Visualization VI, 137–41. Berlin, Heidelberg: Springer Berlin Heidelberg, 1992. http://dx.doi.org/10.1007/978-3-642-84824-7_20.

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Ginevsky, A. S., Ye V. Vlasov, and R. K. Karavosov. "Subsonic Turbulent Jets." In Foundations of Engineering Mechanics, 1–32. Berlin, Heidelberg: Springer Berlin Heidelberg, 2004. http://dx.doi.org/10.1007/978-3-540-39914-8_1.

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Chanetz, Bruno, Jean Délery, Patrick Gilliéron, Patrick Gnemmi, Erwin R. Gowree, and Philippe Perrier. "Subsonic Wind Tunnels." In Springer Tracts in Mechanical Engineering, 51–95. Cham: Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-35562-3_3.

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Gülçat, Ülgen. "Subsonic and Supersonic Flows." In Fundamentals of Modern Unsteady Aerodynamics, 129–69. Berlin, Heidelberg: Springer Berlin Heidelberg, 2010. http://dx.doi.org/10.1007/978-3-642-14761-6_5.

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Gülçat, Ülgen. "Subsonic and Supersonic Flows." In Fundamentals of Modern Unsteady Aerodynamics, 139–83. Cham: Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-60777-7_5.

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Gülçat, Ülgen. "Subsonic and Supersonic Flows." In Fundamentals of Modern Unsteady Aerodynamics, 137–80. Singapore: Springer Singapore, 2015. http://dx.doi.org/10.1007/978-981-10-0018-8_5.

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Mohaghegh, Michael, David L. Stone, Antonio F. Avila, and Keith B. Bowman. "Subsonic Aircraft Materials Development." In Aerospace Materials and Applications, 305–402. Reston ,VA: American Institute of Aeronautics and Astronautics, Inc., 2018. http://dx.doi.org/10.2514/5.9781624104893.0305.0402.

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Ingenito, Antonella. "Ramjets Fuels." In Subsonic Combustion Ramjet Design, 35–45. Cham: Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-66881-5_5.

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Conference papers on the topic "Subsonic"

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Wakayama, Sean. "Subsonic Multi-Role Aircraft." In 44th AIAA Aerospace Sciences Meeting and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2006. http://dx.doi.org/10.2514/6.2006-1513.

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Tangirala, Venkat, Nobuyuki Tsuboi, and Koichi Hayashi. "Performance Estimations for Subsonic-to-Subsonic Flight Conditions of a Pulse Detonation Engine." In 46th AIAA Aerospace Sciences Meeting and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2008. http://dx.doi.org/10.2514/6.2008-113.

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CLEVER, W. "Subsonic/supersonic linear unsteady analysis." In 3rd Applied Aerodynamics Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1985. http://dx.doi.org/10.2514/6.1985-4059.

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Tambe, Samir, San-Mou Jeng, Hukam Mongia, and George Hsiao. "Liquid Jets in Subsonic Crossflow." In 43rd AIAA Aerospace Sciences Meeting and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2005. http://dx.doi.org/10.2514/6.2005-731.

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Khalid, Syed J. "Performance Enhancement of Subsonic Turbofans." In SAE 2016 Aerospace Systems and Technology Conference. 400 Commonwealth Drive, Warrendale, PA, United States: SAE International, 2016. http://dx.doi.org/10.4271/2016-01-2018.

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MORRISON, GERALD, and GARY TATTERSON. "Rectangular subsonic jet flowfield study." In 11th Aeroacoustics Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1987. http://dx.doi.org/10.2514/6.1987-2732.

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Cavalieri, André, Peter Jordan, Tim Colonius, and Yves Gervais. "Axisymmetric superdirectivity in subsonic jets." In 17th AIAA/CEAS Aeroacoustics Conference (32nd AIAA Aeroacoustics Conference). Reston, Virigina: American Institute of Aeronautics and Astronautics, 2011. http://dx.doi.org/10.2514/6.2011-2743.

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Beránek, Jaroslav, and Karel Rohlena. "Magnetic modulation of subsonic COIL." In 18th International Symposium on Gas Flow & Chemical Lasers & High Power Lasers, edited by Tanja Dreischuh, Petar A. Atanasov, and Nikola V. Sabotinov. SPIE, 2010. http://dx.doi.org/10.1117/12.880975.

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VALAREZO, W., and J. HESS. "Time-averaged subsonic propeller flowfield calculations." In 4th Applied Aerodynamics Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1986. http://dx.doi.org/10.2514/6.1986-1807.

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Nathman, James K. "Subsonic Panel Methods - Second (Order) Thoughts." In World Aviation Congress & Exposition. 400 Commonwealth Drive, Warrendale, PA, United States: SAE International, 1998. http://dx.doi.org/10.4271/985563.

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Reports on the topic "Subsonic"

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Alexander, Michael G. Subsonic Wind Tunnel Testing Handbook. Fort Belvoir, VA: Defense Technical Information Center, May 1991. http://dx.doi.org/10.21236/ada240263.

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Chamuel, Jacques R. Littoral Subsonic Seismoacoustic Phenomena Ultrasonic Modeling. Fort Belvoir, VA: Defense Technical Information Center, September 1999. http://dx.doi.org/10.21236/ada630606.

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Chamuel, Jacques R. Littoral Subsonic Seismoacoustic Phenomena Ultrasonic Modeling: Part 1. Fort Belvoir, VA: Defense Technical Information Center, September 1997. http://dx.doi.org/10.21236/ada634011.

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Sherrouse, Peter M. Subsonic Choked Flow LDV Calibrator/Velocity Standard Development. Fort Belvoir, VA: Defense Technical Information Center, February 1985. http://dx.doi.org/10.21236/ada539257.

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Brown, Frank S. Subsonic Relationships between Pressure Altitude, Calibrated Airspeed, and Mach Number. Fort Belvoir, VA: Defense Technical Information Center, September 2012. http://dx.doi.org/10.21236/ada569074.

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Spangler, Sam. Software for Real-Time Analysis of Subsonic Test Shot Accuracy. Fort Belvoir, VA: Defense Technical Information Center, March 2014. http://dx.doi.org/10.21236/ada601466.

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DeSpirito, James. CFD Prediction of Magnus Effect in Subsonic to Supersonic Flight. Fort Belvoir, VA: Defense Technical Information Center, September 2009. http://dx.doi.org/10.21236/ada508090.

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Catalano, George D., Walter B. Sturek, and Sr. A Numerical Investigation of Subsonic and Supersonic Flow Around Axisymmetric Bodies. Fort Belvoir, VA: Defense Technical Information Center, September 2001. http://dx.doi.org/10.21236/ada398641.

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Frampton, Kenneth D., Michael J. Lucas, and Kenneth J. Plotkin. Assessment of the Subsonic Noise Environment in the Nellis Range Complex. Fort Belvoir, VA: Defense Technical Information Center, January 1993. http://dx.doi.org/10.21236/ada405069.

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Dimotakis, Paul E., and Anthony Leonard. Mixing, Chemical Reactions, and Combustion in Subsonic and Supersonic Turbulent Flows. Fort Belvoir, VA: Defense Technical Information Center, September 1998. http://dx.doi.org/10.21236/ada353373.

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