Academic literature on the topic 'Supersonic Business jet'

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Journal articles on the topic "Supersonic Business jet"

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Mirzoyan, Arthur A., Taras Yu Chaika, and Andrey V. Ilyin. "Community Noise Reduction of Supersonic Business Jet." International Journal of Aeroacoustics 3, no. 3 (2004): 289–95. http://dx.doi.org/10.1260/1475472042887470.

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Chudoba, B., G. Coleman, P. A. Czysz, and C. M. Butler. "Feasibility study of a supersonic business jet based on the Learjet airframe." Aeronautical Journal 113, no. 1146 (2009): 517–31. http://dx.doi.org/10.1017/s0001924000003171.

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Abstract Since the dawn of the jet age, passengers on all jet transports, except Concorde, have traveled at about the same speed — a standard Mach 0 83-0 87 range as a practical compromise. After 27 years of supersonic commercial travel, British Airways and Air France retired their fleet of Concorde aircraft at the end of 2003 because it was considered no longer profitable. Clearly, with the retirement of Concorde, the world has lost the only aircraft offering passenger transportation at supersonic speeds. Over the past several years manufacturers have proposed new aircraft designs that promis
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Chudoba, B., G. Coleman, A. Oza, and P. A. Czysz. "What price supersonic speed? A design anatomy of supersonic transportation Part 1." Aeronautical Journal 112, no. 1129 (2008): 141–51. http://dx.doi.org/10.1017/s0001924000002074.

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Abstract The first generation of supersonic commercial transportation has seen three serious attempts to arrive at an economically and environmentally viable aircraft. The US B2707-200/300 design was cancelled early before a prototype could emerge; the Russian Tu-144 design succeeded to become the first supersonic transport but spanned only a few years of restricted airline service; the Anglo-French Concorde endured more than 27 glamorous airline service years until the last of its species was retired on 30 August 2003. This first generation was followed by a second generation of supersonic co
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Berton, J. J., S. M. Jones, J. A. Seidel, and D. L. Huff. "Noise predictions for a supersonic business jet using advanced take-off procedures." Aeronautical Journal 122, no. 1250 (2018): 556–71. http://dx.doi.org/10.1017/aer.2018.6.

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ABSTRACTSupersonic civil aircraft present a unique noise certification challenge. High specific thrust required for supersonic cruise results in high engine exhaust velocity and high levels of jet noise during take-off. Aerodynamics of thin, low-aspect-ratio wings equipped with relatively simple flap systems deepen the challenge. Advanced noise reduction procedures have been proposed for supersonic aircraft. These procedures promise to reduce certification noise levels, but they may require departures from normal reference procedures defined in noise regulations. The subject of this article is
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Chudoba, B., A. Oza, G. Coleman, and P. A. Czysz. "What price supersonic speed? an applied market research case study Part 2." Aeronautical Journal 112, no. 1130 (2008): 219–31. http://dx.doi.org/10.1017/s0001924000002165.

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Abstract The first supersonic business jet to enter the market will not face its competition from rival supersonic designs under development. Its true competitors are the then current generation of highly evolved high-subsonic business jets when compared on economic grounds. For a price tag of $1m for the new conception of very light jets, ranging up to $45m for the highest-performing ‘race-horse’-like corporate jets, this breed of aircraft is able to accommodate the needs of most executives, VIPs, officials, from corporate transportation to cargo services of civil to military origin. Understa
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Sun, Yicheng, and Howard Smith. "Review and prospect of supersonic business jet design." Progress in Aerospace Sciences 90 (April 2017): 12–38. http://dx.doi.org/10.1016/j.paerosci.2016.12.003.

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Smith, H. "A review of supersonic business jet design Issues." Aeronautical Journal 111, no. 1126 (2007): 761–76. http://dx.doi.org/10.1017/s0001924000001883.

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Abstract Key issues relating to the Supersonic Business Jet (SBJ) concept are reviewed with the intent to assess the readiness of enabling technologies and hence the concept itself. The multidisciplinary nature of aircraft design precludes an in-depth analysis of each specific aspect, which could individually be the subject of a separate discipline review, hence an overview is presented. The review looks at the market, environmental issues, with particular reference to the sonic boom phenomenon & solutions, technological issues, including prediction methods, flight testing, systems, ce
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Martins, Joaquim R. R. A., Juan J. Alonso, and James J. Reuther. "High-Fidelity Aerostructural Design Optimization of a Supersonic Business Jet." Journal of Aircraft 41, no. 3 (2004): 523–30. http://dx.doi.org/10.2514/1.11478.

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Freiherr, Greg. "Back to the Sound Barrier." Mechanical Engineering 138, no. 03 (2016): 36–41. http://dx.doi.org/10.1115/1.2016-mar-2.

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This article explores efforts that are being put into developing a business jet called AS2 and various challenges in developing the same. Aerion’s 12-seat tri-engine AS2, unveiled in spring 2014, is designed to have a range up to 5000 nautical miles; reach 51,000 feet; and cruise at speeds between Mach 1.2 and Mach 1.6. About the time it is ready to fly commercially, possibly as early as 2023, the market could support annual sales of 30 supersonic business jets. NASA and Lockheed Martin have been exploring a variety of options for quieting sonic booms. In its Strategic Implementation Plan, rel
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Sun, Y., and H. Smith. "Low-boom low-drag solutions through the evaluation of different supersonic business jet concepts." Aeronautical Journal 124, no. 1271 (2019): 76–95. http://dx.doi.org/10.1017/aer.2019.131.

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ABSTRACTThis paper evaluates six supersonic business jet (SSBJ) concepts in a multidisciplinary design analysis optimisation (MDAO) environment in terms of their aerodynamics and sonic boom intensities. The aerodynamic analysis and sonic boom prediction are investigated by a number of conceptual-level numerical approaches. The panel method PANAIR is integrated to perform automated aerodynamic analysis. The drag coefficient is corrected by the Harris wave drag formula and form factor method. For sonic boom prediction, the near-field pressure is predicted through the Whitham F-function method. T
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Dissertations / Theses on the topic "Supersonic Business jet"

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Borillo, Llorca Irene. "CFD Analysis and Assessment of the Stability and Control of a Supersonic Business Jet." Thesis, KTH, Flygdynamik, 2015. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-180249.

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Extensive research has been done on the aerodynamics of supersonic aircrafts, especially in the military and commercial airplanes’ field. Regarding supersonic business jets (SSBJs), two major problems have been addressed in past investigations: reducing the sonic boom and decreasing the NOx emissions. This report focuses on a di˙erent aspect, the controls and stability of this type of aircrafts. This field has not been addressed thoroughly by the di˙erent companies and universities investigating SSBJs, as most of the existing concepts are preliminary designs that have not been developed extens
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Kincová, Daniela. "Zavedení a provoz supersonického business jetu." Master's thesis, Vysoké učení technické v Brně. Fakulta strojního inženýrství, 2015. http://www.nusl.cz/ntk/nusl-232021.

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Tato práce se zabývá problematikou zavedení a provozu nadzvukových business jetů. V dnešní době se v civilní letecké přepravě, po ukončení provozu Concordu, žádná nadzvuková letadla nevyskytují. V dnešní době existuje mnoho projektů a organizací, které se zabývají znovuzavedením nadzvukových letounů do civilního letectví a soustředí se převážně na business jety. Hlavní otázkou je, zda je vůbec vhodné, či rozumné se k tomu typu dopravy znovu vracet. Existuje hodně problémů, které toto komplikují. Tyto letouny způsobují příliš velký hluk, mají obrovskou spotřebu paliva a musí řešit nadměrné emis
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Books on the topic "Supersonic Business jet"

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Center, NASA Glenn Research, ed. Conceptual design of a supersonic business jet propulsion system. National Aeronautics and Space Administration, Glenn Research Center, 2002.

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L, Beissner F., and United States. National Aeronautics and Space Administration, eds. Effect of emerging technology on a convertible, business/interceptor, supersonic-cruise jet. National Aeronautics and Space Administration, 1986.

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Hensley, Colleen, and Bill Hensley. Pilot--Learning Leadership: Applying Supersonic Jet Flying Principles to Business and Life. Greenleaf Book Group, 2011.

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The Pilot Learning Leadership Applying Supersonic Jet Flying Principles To Business And Life. Greenleaf Book Group, 2011.

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Center, NASA Glenn Research, ed. First order ozone impact of a fleet of supersonic business jets (SSBJs). National Aeronautics and Space Administration, Glenn Research Center, 2002.

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Center, NASA Glenn Research, ed. First order ozone impact of a fleet of supersonic business jets (SSBJs). National Aeronautics and Space Administration, Glenn Research Center, 2002.

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Conference papers on the topic "Supersonic Business jet"

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Sakata, Kimio. "Japan's Supersonic Technology and Business Jet Perspectives." In 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. American Institute of Aeronautics and Astronautics, 2013. http://dx.doi.org/10.2514/6.2013-21.

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Schutte, Jeffrey S., Dimitri N. Mavris, and Michelle R. Kirby. "Technology Assessment of a Supersonic Business Jet." In Aerospace Technology Conference and Exposition. SAE International, 2005. http://dx.doi.org/10.4271/2005-01-3393.

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Daumas, Laurent, Nicolas Heron, Zdenek Johan, Gilbert Roge, and Sebastien Vigneron. "Aerodynamic Design Process of a Supersonic Business Jet." In 24th AIAA Applied Aerodynamics Conference. American Institute of Aeronautics and Astronautics, 2006. http://dx.doi.org/10.2514/6.2006-3459.

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Rallabhandi, Sriram, and Dimitri Mavris. "Design and Analysis of Supersonic Business Jet Concepts." In 6th AIAA Aviation Technology, Integration and Operations Conference (ATIO). American Institute of Aeronautics and Astronautics, 2006. http://dx.doi.org/10.2514/6.2006-7702.

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Kiyici, Firat, and Selin Aradag. "Design and Optimization of a Supersonic Business Jet." In 22nd AIAA Computational Fluid Dynamics Conference. American Institute of Aeronautics and Astronautics, 2015. http://dx.doi.org/10.2514/6.2015-3064.

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Stone, James, Eugene Krejsa, Ian Halliwell, and Bruce Clark. "Noise suppression nozzles for a supersonic business jet." In 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. American Institute of Aeronautics and Astronautics, 2000. http://dx.doi.org/10.2514/6.2000-3194.

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Bruckner, Robert. "Conceptual Design of a Supersonic Business Jet Propulsion System." In 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. American Institute of Aeronautics and Astronautics, 2002. http://dx.doi.org/10.2514/6.2002-3919.

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Sturdza, Peter. "Extensive Supersonic Natural Laminar Flow on the Aerion Business Jet." In 45th AIAA Aerospace Sciences Meeting and Exhibit. American Institute of Aeronautics and Astronautics, 2007. http://dx.doi.org/10.2514/6.2007-685.

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Gonzalez Gallego, Oscar, Ruben E. Perez, and Peter W. Jansen. "Technical Viability and Operational Assessment of a Supersonic Business Jet." In 2018 Aviation Technology, Integration, and Operations Conference. American Institute of Aeronautics and Astronautics, 2018. http://dx.doi.org/10.2514/6.2018-3661.

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Agte, Jeremy S., Jaroslaw Sobieszczanski-Sobieski, and Robert R. Sandusky. "Supersonic Business Jet Design Through Bi-Level Integrated System Synthesis." In World Aviation Congress & Exposition. SAE International, 1999. http://dx.doi.org/10.4271/1999-01-5622.

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