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Journal articles on the topic 'Supersonic Business jet'

Author: Grafiati

Published: 4 June 2021

Last updated: 10 February 2022

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1

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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2

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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3

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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4

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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5

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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6

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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7

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 &amp; solutions, technological issues, including prediction methods, flight testing, systems, ce

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8

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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9

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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10

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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11

Abdalla, Alvaro Martins, Felipe de Castro Baraky, and Matheus Urzedo Quirino. "Conceptual design analysis of a variable swept half-span wing of a supersonic business jet." CEAS Aeronautical Journal 11, no. 4 (2020): 885–95. http://dx.doi.org/10.1007/s13272-020-00457-8.

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12

SATO, Koma, Takayasu KUMANO, Masahito YONEZAWA, Hiroshi YAMASHITA, Shinkyu JEONG, and Shigeru OBAYASHI. "Low-Boom and Low-Drag Optimization of the Twin Engine Version of Silent Supersonic Business Jet." Journal of Fluid Science and Technology 3, no. 4 (2008): 576–85. http://dx.doi.org/10.1299/jfst.3.576.

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13

Ilyin, Andrey V., Taras Yu Chaika, Artur A. Mirzoyan, Igor N. Egorov, and Gennady V. Kretinin. "Robust Optimization of Integrated Aircraft-Propulsion System Control to Meet Takeoff Noise Requirements of Supersonic Business Jet." International Journal of Aeroacoustics 3, no. 3 (2004): 271–87. http://dx.doi.org/10.1260/1475472042887506.

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14

Grewe, V., A. Stenke, M. Plohr, and V. D. Korovkin. "Climate functions for the use in multi-disciplinary optimisation in the pre-design of supersonic business jet." Aeronautical Journal 114, no. 1154 (2010): 259–69. http://dx.doi.org/10.1017/s0001924000003705.

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Abstract Mitigation of climate change is a challenge to science and society. Here, we establish a methodology, applicable in multi-disciplinary optimisation (MDO) during aircraft pre-design, allowing a minimisation of the aircraft’s potential climate impact. In this first step we consider supersonic aircraft flying at a cruise altitude between 45kfeet (~13·5km, 150hPa) and 67kfeet (~20·5km, 50hPa). The methodology is based on climate functions, which give a relationship between 4 parameters representing an aircraft/engine configuration and an expected impact on global mean near surface tempera

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15

Liu, Shaowei, Junqiang Bai, Peixun Yu, Bao Chen, and Boxiao Zhou. "Aerodynamic Optimization Design on Supersonic Transports Considering Sonic Boom Intensity." Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University 38, no. 2 (2020): 271–78. http://dx.doi.org/10.1051/jnwpu/20203820271.

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It is key points to improve the aerodynamic efficiency and decrease the sonic-boom intensity for the supersonic aircraft design. Sonic-boom prediction method with high precision combining the near-field sonic-boom prediction based on Reynolds-Averaged Navier-Stokes equations and the far-field sonic-boom prediction based on waveform parameter method is firstly established. Then the gradient of sonic boom with respect to the design variables is calculated by the finite difference method and is combined with the gradient of the aerodynamic object by the discrete adjoint technique, acting as the g

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16

Sun, Yicheng, and Howard Smith. "Design and operational assessment of a low-boom low-drag supersonic business jet." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, April 9, 2021, 095441002110080. http://dx.doi.org/10.1177/09544100211008041.

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There has been a worldwide interest to develop a supersonic business jet (SSBJ) for a minimum range of 4000 nm with low sonic boom intensity and high fuel efficiency. An SSBJ design model is developed in the GENUS aircraft conceptual design environment. With the design model, a low-boom low-drag SSBJ concept is designed and optimized. This article studies the design concept for its operational performances. The sustained supersonic cruise flight is studied to find out the fuel-efficient Mach number and altitude combinations. The combined supersonic and subsonic cruise flight scenarios are stud

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17

Behdinan, Kamran, Ruben E. Perez, and Hugh T. Liu. "MULTIDISCIPLINARY DESIGN OPTIMIZATION OF AEROSPACE SYSTEMS." Proceedings of the Canadian Engineering Education Association (CEEA), August 15, 2011. http://dx.doi.org/10.24908/pceea.v0i0.3914.

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This paper presents the evaluation of different MDO methodologies which take into consideration optimization and other factors influencing their structures. Illustrative comparisons are made for analytic functions and a supersonic business jet design case study. Results show the promising features of the proposed evaluation metrics to define a standardized guideline when dealing with multidisciplinary optimization formulations which can be applied to aerospace systems design problems.

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18

Brezillon, Joël, Gerald Carrier, and Martin Laban. "Multidisciplinary Optimization of Supersonic Aircraft Including Low-Boom Considerations." Journal of Mechanical Design 133, no. 10 (2011). http://dx.doi.org/10.1115/1.4004972.

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This paper presents a multidisciplinary optimization framework developed by the authors and applied to small-size supersonic aircraft. The multidisciplinary analysis suite is based on the combination of low (empirical) and high-fidelity computational fluid dynamics (CFD) and computational structure mechanics (CSM) tools for predicting the overall aircraft performance and the sonic boom overpressure at supersonic flight, which represents the most challenging environmental constraint for supersonic aircraft. The analysis suite is coupled with a multi-objective optimization strategy for quantifyi

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19

Tosserams, S., M. Kokkolaras, L. F. P. Etman, and J. E. Rooda. "A Nonhierarchical Formulation of Analytical Target Cascading." Journal of Mechanical Design 132, no. 5 (2010). http://dx.doi.org/10.1115/1.4001346.

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Analytical target cascading (ATC) is a method developed originally for translating system-level design targets to design specifications for the components that comprise the system. ATC has been shown to be useful for coordinating decomposition-based optimal system design. The traditional ATC formulation uses hierarchical problem decompositions, in which coordination is performed by communicating target and response values between parents and children. The hierarchical formulation may not be suitable for general multidisciplinary design optimization (MDO) problems. This paper presents a new ATC

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20

Yurchenko, Nina F., David S. Breed, and Shaowei Zhang. "Design of the Airbag Inflation System Applicable to Conventional and Autonomous Vehicles." Automotive Innovation, September 13, 2021. http://dx.doi.org/10.1007/s42154-021-00156-y.

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AbstractThe emergency transformation of various aspects of life and business these days requires prompt evaluation of autonomous vehicles. One of the primary reassessments deals with the applicability of the vehicle passive safety system to the protection of arbitrarily positioned passengers. To mitigate possible risks caused by the simultaneous deployment of several big airbags, a new principle of their operation is required. Herein, the aspirated inflator for a driver airbag is developed that can provide 50L-airbag inflation within 30–40 ms. As a result, about 3/4 of the air is to be entrain

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