Overcoming sonic boom for supersonic business jets

• Autorzy: Skalski P. , Pakulski T.

Warianty tytułu

PL

Przezwyciężenie bariery dźwięku dla nadźwiękowych małych samolotów pasażerskich

• Języki publikacji: EN

Abstrakty

EN

Following a discussion of the role of sonic boom in limiting the progress of commercial supersonic flight, a review of existing and developing initiatives to overcome this problem is presented. The paper evaluates the relevance of competing public and private sector research on overcoming sonic boom to the development of Supersonic Business Jets, in the context of a restrictive legal situation. A perspective on the likely technology incorporated in future Supersonic Business Jets is presented.

PL

W pracy przeprowadzono dyskusję na temat roli bariery dźwięku w ograniczeniu postępu naddźwiękowego lotu komercyjnego. Dokonano przeglądu istniejących i rozwijanych inicjatyw przezwycieżenia tego problemu. Praca ocenia znaczenie konkurencyjnych badań publicznych i prywatnych celem rozwoju naddźwiękowych małych samolotów pasażerskich, w kontekście restrykcyjnej sytuacji prawnej. Perspektywa na rozwój technologii pozwalającej na podróż naddźwiękowymi małymi samolotami pasażerskimi została zaprezentowana.

Słowa kluczowe

EN

sonic boom; supersonic flight; Supersonic Business Jets

PL

bariera dźwięku; lot naddźwiękowy; samolot pasażerski

• Wydawca: Sieć Badawcza Łukasiewicz - Poznański Instytut Technologiczny
• Czasopismo: Logistyka
• Rocznik: 2014
• Tom: nr 6
• Strony: 9562--9569
• Opis fizyczny: Bibliogr. 29 poz., pełny tekst na CD3

Twórcy

autor

Skalski P.

• Institute of Aviation, Centre of New Technologies; 02-256 Warsaw; Al. Krakowska 110/114

autor

Pakulski T.

• University of Bath; Department of Mechanical Engineering; United Kingdom

Bibliografia

• 1. N. R. C. Committee on Breakthrough Technology for Commercial Supersonic Aircraft, Commercial Supersonic Technology - The Way Ahead, Washington, D.C.: National Academies Press, 2001.
• 2. K. L. B. Liebhardt, “An Analysis of the Market Environment for Supersonic Business jets,” German Aerospace Center (DLR) – Air Transportation Systems,, Hamburg.
• 3. W. H. Andrews, “Summary of Prelimenary Data Derived from the XB-70 Airplanes,” NASA, Washington, D.C., 1966.
• 4. USAF, “USAF Fact Sheet 96-03,” Armstrong Laboratory, 1996.
• 5. J. M. Sands, “Sonic Boom Research 1958-1968,” Federal Aviation Administration, Department of Transportation, Washington, D.C., 1968.
• 6. P. J. J. J. R. Y. K. O. KRYTER, “Psychological Experiments on Sonic Booms Conducted at Edwards Air Force Base,” Stanford Research Institute, Menlo Park, California, 1968.
• 7. A. Busemann, “The Relation between Minimizing Drag and Noise at Supersonic Speeds,” Proceedings of High Speed Aerodynamics, pp. 133-144, 1955.
• 8. A. E. W. L. G. H. R. G. B. D. C. E. S. S. L. P. N. M. H. A. M. R. MCgowan, “Recent results from NASA's Morphing Project,” Smart Structures and Materials, 2002.
• 9. R. Dorr, “F-14 Tomcat: Fleet Defender,” World Air Power Journal , pp. 42-99, 1991.
• 10. M. Spick, The Great Book of Modern Warplanes, St. Paul, Minnesota : MBI Publishing Company, 2000.
• 11. NASA, “Oblique Wing Research Aircraft,” NASA, [Online]. Available: http://www.nasa.gov/centers/dryden/about/Organizations/Technology/Facts/TF-2004-01-DFRC_prt.htm. [Accessed 26 August 2013].
• 12. J. E. I. B. K. P. P. W. C. Thill, “Morphing Skins,” The Aeronautical Journal, pp. 1-23, March 2008.
• 13. D. S. E. B. H. P. Monner, “Design Aspects of the Elastic Trailing Edge for an Adaptive Wing,” Aeronaut J., pp. 89-95, 2000.
• 14. J. Kurzke, “The Mission Defines the Cycle: Turbojet, Turbofan and Variable Cycle Engines for High Speed Propulsion,” NATO.
• 15. D. A. J. J. Thibert, “A review of ONERA aerodynamic research in support of a future supersonic transport aircraft,” Progress in Aerospace Sciences , pp. 581-627, November 2000.
• 16. R. D. B. R. J. C. G. A. F. T. L. Turner, “Design, fabrication, and testing of SMA enabled adaptive chevrons for jet noise reduction,” NASA, Langley, 2004.
• 17. L. S. Works, “SR-71 Manual,” sr-71.org.
• 18. R. Seebass, “Sonic Boom Minimization,” NATO, 1998.
• 19. J. D. Leatherwood and B. M. Sullivan, “aboratory study of effects of sonic boom shaping on subjective loudness and acceptability,” NASA, Langley, VA, 2003.
• 20. D. H. G. C. H. B. P. G. C. D. J. M. Joseph W. Pawlowski, “Origins and Overview of the Shaped Sonic Boom Demonstration Program,” American Institute of Aeronautics and Astronautics , 2005.
• 21. G. C. Beth Dickey, “RELEASE : 09-016 - Lancets Flights Probe Supersonic Shockwaves,” NASA, 22 January 2009. [Online]. Available: http://www.nasa.gov/home/hqnews/2009/jan/HQ_09016_Lancet_flights.html. [Accessed 28 August 2013 ].
• 22. Dryden Flight Research Center, Edwards, California, “Analysis of Nozzle Jet Plume Effects on Sonic Boom Signature,” NASA Tech Briefs , 2010.
• 23. “Aerion's Supersonic Business Jet,” Aerion Corp. , [Online]. Available: http://aerioncorp.com/jet. [Accessed 22 August 2013].
• 24. E. Hagerman, “Supersonic jet promises to fly nearly silent,” CNN, 16 February 2007. [Online]. Available: http://edition.cnn.com/2007/TECH/02/16/quiet.supersonic/index.html. [Accessed 22 August 2013].
• 25. C. F. B. A. M. N. K. Maute, “Sonic Boom Mitigation via Shape Optimisatino Using an Adjoint Method and Application to a Supersonic Fighter Aircraft,” REMN, 2006.
• 26. “NASA Investigates the 'FaINT' Side of Sonic Booms,” NASA, 31 October 2012. [Online]. Available: http://www.nasa.gov/topics/aeronautics/features/faint_sonic_booms.html#.Uhs54Bt7JU8. [Accessed 26 August 2013].
• 27. D. H. Martina Kästner, “Sound Propogation of Sonic Booms through Real Atmospheres Emitted from a New Supersonic Business Craft,” Institute of Atmospheric Physics, German Aerospace Center, Oberpfaffenhofen, Germany.
• 28. M. Belfiore, “The Return of the Supersonic Biplane,” PopularMechanics, 21 March 2012. [Online]. Available: http://www.popularmechanics.com/technology/aviation/news/the-return-of-the-supersonic-biplane-7505124. [Accessed 27 August 2013].
• 29. K. M. D. M. Kazuhiro Kusunosea, “Supersonic biplane—A review,” Progress in Aerospace Sciences, 19 November 2010.