Multi-objective optimization of turbofan design parameters for an advanced, single-aisle transport

10th AIAA Aviation Technology, Integration and Operations Conference 2010, ATIO 2010

Volumn 2, Issue , 2010, Pages

  Berton, Jeffrey J ^a   Guynn, Mark D ^b  

^a NASA GLENN RESEARCH CENTER   (United States)

^b NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC DESIGNS; AIRCRAFT DESIGNERS; COMMERCIAL TRANSPORT; FAN PRESSURE RATIO; OBJECTIVE FUNCTIONS; OPTIMIZED SOLUTIONS; OVERALL PRESSURE RATIOS; TECHNOLOGY DEVELOPMENT;

ALGORITHMS; AVIATION; BYPASS RATIO; CONCEPTUAL DESIGN; ENGINES; FIXED WINGS; MACHINE DESIGN; MULTIOBJECTIVE OPTIMIZATION; NASA;

AIRCRAFT;

EID: 84878467073     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2010-9168     Document Type: Conference Paper

References (37)

1. Guynn, M.D., Berton, J.J., Fisher, K.L., Haller, W.J., Tong, M.T., and Thurman, D.R.: "Engine Concept Study for an Advanced Single-Aisle Transport," NASA TM-2009-215784, August, 2009.
2. Guynn, M.D., Berton, J.J., Fisher, K.L., Haller, W.J., Tong, M.T., and Thurman, D.R.: "Analysis of Turbofan Design Options for an Advanced Single-Aisle Transport Aircraft," 9th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference, September, 2009.
3. Guynn, M.D., Berton, J.J., Fisher, K.L., Haller, W.J., Tong, M.T., and Thurman, D.R.: "Refined Exploration of Turbofan Design Options for an Advanced Single-Aisle Transport," NASA TM to be published, 2010.
4. Berton, J.; Envia, E.; and Burley, C.: "An Analytical Assessment of NASA's N+1 Subsonic Fixed Wing Project Noise Goal," AIAA Paper 2009-3144, 15th AIAA/CEAS Aeroacoustics Conference (30th AIAA Aeroacoustics Conference), Miami, FL, 11-13 May, 2009.
5. Norris, G.; and Wall, R.: "Boeing Goes Back to Drawing Board for 737 Follow-on," Aviation Week and Space Technology, 18 May, 2008.
6. Polek, G.: "Boeing, Airbus Commit to Re-engining Decisions by Year-end," Aviation International News, 26 February, 2010.
7. Claus, R.W.; Evans, A.L.; Lytle, J.K., and Nichols, L.D.: "Numerical Propulsion System Simulation," Computing Systems in Engineering, Vol. 2, No. 4, pp. 357-364, 1991.
8. NPSS User Guide Software Release: NPSS_1.6.5.
9. Onat, E., and Klees, G.: "A Method to Estimate Weight and Dimensions of Large and Small Gas Turbine Engines," NASA CR 159481, 1979.
10. McCullers, L.A.: "Aircraft Configuration Optimization Including Optimized Flight Profiles," Proceedings of the Symposium on Recent Experiences in Multidisciplinary Analysis and Optimization, NASA CP 2327, April 1984.
11. Ardema, M.D., Chambers, M.C., Patron, A.P, Hahn, A.S., Miura, H., and Moore, M.D., "Analytical Fuselage and Wing Weight Estimation of Transport Aircraft," NASA TM-110392, May 1996.
12. Jane's Aero-Engines, Jane's Information Group, Alexandria, VA (various).
13. 787 Dreamliner Program Fact Sheet, URL: http://www.boeing.com/commercial/787family/programfacts.html [cited 6/8/2010].
14. J.R.; Davis, P.C.; and Gelhausen, P.A.: "A Rapid Geometry Modeler for Conceptual Aircraft," AIAA-1996-0052, January, 1996.
15. U.S. Code of Federal Regulations, Title 14, Chapter I, Part 25. Airworthiness Standards: Transport Category Airplanes.
16. U.S. Code of Federal Regulations, Title 14, Chapter I, Part 36. Noise standards: Aircraft type and airworthiness certification.
17. 737 Airplane Characteristics for Airport Planning," D6-58325-6, Boeing Commercial Airplanes, October 2005.
18. International Standards and Recommended Practices - Environmental Protection, Annex 16 to the Convention on International Civil Aviation, Volume II: Aircraft Engine Emissions, 2nd Edition, International Civil Aviation Organization (ICAO), Montreal, Canada, July 1993.
19. U.S. Code of Federal Regulations, Title 14, Chapter I, Part 34. Fuel Venting and Exhaust Emission Requirements for Turbine Engine-Powered Airplanes.
20. Rink, K.K.; and Lefebvre, A.H.: "The Influence of Fuel Composition and Spray Characteristics on Nitric Oxide Formation," Combustion, Science and Technology, vol. 68, pp. 1-14, 1989.
21. Correa, S.M.: "Lean Premixed Combustion for Gas Turbines: Review and Required Research," Fossil Fuel Combustion, ASME PD-Vol. 33, 1991.
22. Leonard, G.L.; and Correa, S.M.: "NOX Formation in Lean Premixed High-Pressure Methane Flames," Second ASME Fossil Fuel Combustion Symposium, PD-30, pp. 69-74, 1990.
23. Dahl, M.D. (ed.): "Assessment of NASA's Aircraft Noise Prediction Capability," NASA TP-20 XX-215653, to be published.
24. Gillian, R.E.: "Aircraft Noise Prediction Program User's Manual," NASA TM-84486, 1983.
25. Zorumski, W.E.: "Aircraft Noise Prediction Program Theoretical Manual," NASA TM-83199, 1981, Parts 1 and 2 (Currently maintained at NASA Langley Research Center by the ANOPP team in electronic format and provided upon request; Latest revision: January 2009).
26. Kontos, K.B.; Janardan, B.; and Gliebe, P.R.: "Improved NASA-ANOPP Noise Prediction Computer Code for Advanced Subsonic Propulsion Systems Volume 1: ANOPP Evaluation and Fan Noise Model Improvement," NASA CR-195480, 1996.
27. Stone, J.R., Krejsa, E.A., Clark, B.J., and Berton, J.J.: "Jet Noise Modeling for Suppressed and Unsuppressed Aircraft in Simulated Flight," NASA TM-2009-215524, 2009.
28. Emmerling, J.J.; Kazin, S.B.; and Matta, R.K.: "Core Engine Noise Control Program. Volume III, Supplement 1 - Prediction Methods," FAA-RD-74-125, III-I, Mar. 1976 (Available from DTIC as AD A030 376.)
29. Ho, P.Y.; and Doyle, V.L.: "Combustion noise prediction update," 5th AIAA Aeroacoustics Conference, Seattle, WA, AIAA Paper 1979-0588, 1979.
30. Jones, M.; Parrott, T.; Sutliff, D.; Hughes, C.: "Assessment of Soft Vane and Metal Foam Engine Noise Reduction Concepts," 15th AIAA/CEAS Aeroacoustics Conference, AIAA-2009-3142, 2009.
31. Sutliff, D.L.; Jones, M.G.; and Hartley, T.C.: "Attenuation of FJ44 Turbofan Engine Noise with a Foam-Metal Liner Installed Over-the-Rotor," 15th AIAA/CEAS Aeroacoustics Conference (30th AIAA Aeroacoustics Conference), Miami, FL, AIAA Paper 2009-3141, 2009.
32. Fink, M.R.: "Airframe Noise Prediction Method," FAA-RD-77-29, March, 1977.
33. Humphries, W.M.; Burley, C.L.; and Brooks, T.F.: "Scale-Model Landing Gear Noise Spectra and Directivity," Acoustics Technical Working Group Meeting, 23-24 Sep. 2008, Williamsburg, VA, United States.
34. Envia, Edmane: "Progress Toward N+1 Noise Goal," Fundamental Aeronautics Program, Subsonic Fixed Wing Project, 12-Month Program Review, Washington, DC, November 5-6, 2008.
35. Deb, K.; Pratap, A.; Agarwal, S.; and Meyarivan, T.: "A Fast and Elitist Multi-Objective Genetic Algorithm: NSGA-II," IEEE Transactions on Evolutionary Computation, vol. 6, no. 2, pp. 181-197, 2002.
36. Deb, K.; and Agrawal, R. B.: "Simulated Binary Crossover for Continuous Search Space," Complex Systems, vol. 9, no. 2, pp. 115-148, 1995.
37. Deb, K.; Pratap, A.; and Meyarivan, T.: "Constrained Test Problems for Multi-objective Evolutionary Optimization," Proceedings of the First International Conference on Evolutionary Multi-Criterion Optimization, Zurich, Switzerland, pp. 284-298, March 7-9, 2001.