Aerodynamics for revolutionary air vehicles

21st AIAA Applied Aerodynamics Conference

Volumn , Issue , 2003, Pages

  Sellers III, William L ^a,b   Singer, Bart A ^a,c   Leavitt, Laurence D ^a,d  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b Physics and Control Branch   (United States)

^c Computational Modeling and Simulation ^*  (United States)

^d Configuration Aerodynamics Branch ^*  (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AIR TRANSPORTATION; NASA;

AERONAUTICS RESEARCH; AIR VEHICLE; AIRLINE INDUSTRY; DESIGN SPACES; ENVIRONMENTAL ISSUES; INCREMENTAL IMPROVEMENTS; ROADMAPPING;

VEHICLES;

EID: 85067319861     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2003-3785     Document Type: Conference Paper

References (105)

1. Schneider, Wolfgang: "The Importance of Aerodynamics in the Development of Commercially Successful Transport Aircraft", CEAS/DragNet European Drag Prediction Conference 2000, Potsdam, Germany, 19-21 June 2000.
2. Dexter, P. C.: "A Strategic European Approach to Aerodynamics Research, Technology, and Development", Aero Journal, August 2001, pp. 451-457.
3. Group of Personalities, "European Aeronautics: A Vision for 2020 - Meeting Society's Needs and Winning Global Leadership", 2001. Available online at: http://europa.eu.int/comm/research/growth/aeronautics2020/en/
4. "The NASA Aeronautics Blueprint - Toward a Bold New Era of Aviation", 3 Jun. 2002, http://www.aero-space.nasa.gov/aero_blueprint/index.html
5. Abey-Wickrama L.a'Brook, M.F., Gattoni, F.E.G., and Herridge, C.F., Mental hospital admissions and aircraft noise, Lancet 2 pp.1275-1277, 1969.
6. Meecham, W.C., and Shaw, N.A., "Increase in mortality rate due to aircraft noise," Proc. of Inter-Noise 93 Leuven, Belgium, 1993.
7. Powell, C. A. and Preisser, J. S.: "NASA Subsonic Jet Transport Noise Reduction Research", Aero Journal, August 2000, pp. 353-358
8. Schmitt, Dieter: "Challenges for Unconventional Transport Aircraft Configurations", Air and Space Europe, Vol. 3, No. 3/4, 2001pp 67-72
9. Panel on Atmospheric Effects of Aviation: "The Atmospheric Effects of Stratospheric Aircraft Project - An Interim Review of Science an Progress", National Research Council, National Academy Press, Washington, D.C., 1998
10. Intergovernmental Panel on Climate Change: "Aviation and the Global Atmosphere", Cambridge University Press, 1999.
11. Green, J. E.: "Greener by Design - The Technology Challenge", The report by the Technology Sub Group, Aero Journal, February, 2002, pp. 57-106
12. "The Environmental Effects of Civil Aircraft in Flight", Royal Commission on Environ mental Pollution, 2002
13. Arthur D. Little Ltd: "Study into the Potential Impact of Changes in Technology on the Development of Air Transport in the UK", DETR/71861/10rep.doc, 2000
14. Minnis, P., Young D. F., Nguyen L., Garber D. P., Smith Jr., W. L., and Palikonda, R.: "Trans-formation of Contrails into Cirrus During SUCCESS", Geophys. Res. Ltrs., 25, 1157-1160.
15. th Conference on Aviation, Range, and Aerospace Meteorology, Portland, OR, 13-16 May, 2002
16. NASA Press Release No. 02-035, "NASA Scientists Use Empty Skies to Study Climate Change", 13 May, 2002.
17. thAIAA, Aerospace Sciences Meeting & Exhibit, AIAA Paper 98-0135, Reno, NV, Jan. 12-15, 1998
18. Gelsinger, Pat: "Moore's Law Extends and Expands for the Future", available at, http://www.intel.com/labs/eml/painterview.htm
19. "New Transistors for 2005 and Beyond", available online at: http://www.intel.com/research/silicon/micron. htm
20. Gasser, Bob: "Nanotechnology in Electron Devices", American Institute of Chemical Engineers Meeting (AIChE), February, 11, 2003
21. Moravec, Hans: "Robot - Mere Machine to Transcendent Mind", Oxford University Press, 1999
22. Kurzweil, Ray: "The Law of Accelerating Returns", available online at: http://www.kurzweilai.net/articles/art0134.html
23. th Symposium on Computer Architecture and High Performance Computing, Vitoria/ES-Brazil, October 28-30, 2002
24. http://www.top500.org
25. th AIAA Aerospace Sciences Meeting, Reno, NV 14-17 January, 2002
26. McMasters, John H. and Cummings, Russell M.: "Airplane Design - Past, Present, and Future", Journal of Aircraft, Vol. 39, No. 1, Jan-Feb, 2002
27. Dreisbach, Rodney L.: "Trends in the Design Analysis of Aerospace Vehicles", Daratech iDPS 2001 Conference on Intelligent Digital Prototyping Strategies, Novi, MI, 29-30 October, 2001
28. National Research Council, Aeronautics and Space Engineering Board: "Commercial Supersonic Technology: The Way Ahead", National Academy Press, Washington, D.C., 2001
29. Gad-el-Hak, M., "Introduction to Flow Control", in Flow Control: Fundamentals and Practices, Springer-Verlag, 1998, pp. 1-108.
30. Kumar, Ajay, and Hefner, Jerry N.: "Future Challenges and Opportunities in Aerodynamics", Proceedings of the 22nd International Congress of Aeronautical Sciences, Harrogate, U.K., Aug.27-Sept.1, 2000. Also published in The Aeronautical Journal, vol. 104, No. 1038, pp. 365-373, Aug. 2000.
31. Thomas, Russell H., and Choudhari, Meelan M.: "Flow and Noise Control: Review and Assessment of Future Directions", NASA TM-2002-211631, April, 2002
32. Lord, W. K., MacMartin, D. G., and Tillman, T. G.: "Flow Control Opportunities in Gas Turbine Engines", AIAA 2000-2234, Fluids 2000, Denver, CO, 19-22 June, 2000
33. Lin, J. C: "Control of Turbulent Boundary-Layer Separation using Micro-Vortex Generators", AIAA Paper 99-3404, 30th AIAA Fluid Dynamics Conference, Norfolk, VA, June 28-July 1, 1999.
34. Lin, J. C: Review of Research on Low-Profile Vortex Generators to Control Boundary-Layer Separation. Progress in Aerospace Sciences, v. 38, issue 4-5, 2002, pp. 389-420.
35. Walsh, M.J. Riblets, Viscous Drag Reduction in Boundary Layers, Vol. 123, Ed. D.M. Bushnell and J.N. Hefner. Washington, DC:, American Institute of Aeronautics and Astronautics, Inc., 1990, pp 203-261.
36. Walsh, M. J., Sellers, W. L. III, and McGinley, C. B. Riblet Drag at Flight Conditions. Journal of Aircraft, Vol. 26, No. 6, June 1989, Pages 750-755.
37. McLean, J. D., George-Falvy, D. N., and Sullivan, P. P. "Flight -Test of Turbulent Skin Friction Reduction by Riblets," Turbulent Drag Reduction by Passive Means; Proceedings of the International Conference, London, England, Sept. 15-17, 1987. Volume 2. London, Royal Aeronautical Society, 1987, p. 408-424.
38. th Aerospace Sciences Meeting, Reno, Nevada, January 7-10, 1991.
39. Drewer, D.: "Riblets Enter Service", Flight International, Vol. 27, August, 1988
40. Marec, J.-P.: "Drag Reduction: A Major Task for Research", CEAS/DragNet European Drag Reduction Conference, Potsdam, Germany, 19-21 June 2000.
41. "Drag Reducing Riblets" Aerospace Engineering, December, 1989, pp. 39-42.
42. Viswanath, P. R., Aircraft Viscous Drag Reduction Using Riblets. Progress in Aerospace Sciences, Volume 38, pp. 571-600, 2002
43. Saric, W. S., Carrillo, R. B., and Reibert, M. S.: "Leading-Edge Roughness as a Transition Control Mechanism", AIAA 98-0781, AIAA, Aerospace Sciences Meeting & Exhibit, 36th, Reno, NV, Jan. 12-15, 1998
44. st Flow Control Conference, St. Louis, MO, 24-26 June, 2002
45. Joslin, R. D.: "Overview of Laminar Flow Control", NASA TP-1998-208705, 1998
46. Joslin, R. D.: "Aircraft Laminar Flow Control", Annual Review of Fluid Mechanics, Vol. 30, pp.1-29, 1998
47. Arcara, P. C., Jr, Bartlett, D. W., and McCullers, L. A.: "Analysis for the Application of Hybrid Laminar Flow Control to a Long-Range Subsonic Aircraft", SAE Paper 912113, 1991
48. Greenblatt, D. and Wygnanski, I., Control of Separation by Periodic Excitation, Progress in Aerospace Sciences, Volume 36, Issue 7, pp. 487-545, 2000.
49. McLean, J. D., Crouch, J. D., Stoner, R. C., Sakurai, S., Seidel, G. E., Feifel, W. M., and Rush, H. M.: "Study of the Application of Separation Control by Unsteady Excitation to Civil Transport Aircraft", NASA CR-209338, 1999.
50. Englar, R. J.: "Circulation Control Pneumatic Aerodynamics: Blown Force and Moment Augmentation and Modifications; Past, Present, and Future", AIAA Paper 2000-2541, Fluids 2000 Conference and Exhibit, Denver, CO, June 19-22, 2000
51. st AIAA Flow Control Conference, St. Louis, MO, 24-27 June, 2002
52. th AIAA Aerospace Sciences Meeting & Exhibit, Reno, NV, 8-11 January, 2001
53. Stanewsky, E.: "Adaptive Wing and Flow Control Technology", Progress in Aerospace Sciences, Volume 37, Issue 7, pp. 583-667, 2001
54. Breitbach, Elmar J., Anhalt, Christian, and Monner, Hans P.: "Overview of Adaptronics in Aeronautical Applications", Air and Space Europe, Vol. 3, No 3/4, 2001
55. Kroo, Ilan: "Drag Due to Lift: Concepts for Prediction and Reduction", Annual Review of Fluid Mechanics, Vol. 33, 2001, pp. 587-617
56. McMasters J. and Kroo, I.: "Advanced Configurations for Very Large Transport Airplanes", Aircraft Design, 1:217-42
57. "Drag Reduction by Shock Boundary Layer Control - Results of the Project EUROSHOCK II Supported by the European Union 1996-1999", Notes on Numerical Fluid Mechanics and Multidisciplinary Design, Volume 80, eds. Stanewsky, Egon, Delery, Jean, Fulker, John, and Paolo de Matteis, Springer-Verlag, 2002
58. th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference and Exhibit, Long Beach, CA Apr. 20-23, 1998
59. th AIAA Aerospace Sciences Meeting & Exhibit, Reno, NV, 8-11 January, 2001
60. Pasamanick, Jerome, "Langley Full-Scale-Tunnel Tests of the Custer Channel Wing Airplane," NACA RM L53A09, National Advisory Committee for Aeronautics, April, 1953
61. st AIAA Flow Control Conference, St. Louis, MO, 24-27 June, 2002
62. st AIAA Flow Control Conference, St. Louis, MO, 24-27 June, 2002
63. Sellers, William L. III, Jones, Gregory S., and Moore, Mark D.: Flow Control Research at NASA Langley in Support of High-Lift Augmentation, AIAA 2002-6006, Biennial International Powered Lift Conference, Williamsburg, VA, 5-7 November, 2002
64. Pfenninger, W.: "Design Considerations of Large Subsonic Long Range Transport Airplanes with Low Drag Boundary Layer Suction", Report No. NAL-58-529 (BLC-111), 1958, Available from DTCI as AD-821759.
65. Kulfan, Robert M. and Vachal, John D.: "Wing Planform Geometry Effects on Large Subsonic Military Airplanes", AFFDL-TR-78-16, U. S. Air Force, Available from DTIC as AD-A056-124.
66. Gundlach, et.al.: "Conceptual Design Studies of a Strut-Braced Wing Transonic Transport", Journal of Aircraft, Vol. 37, No. 6, Nov-Dec, 2000
67. rd International Congress of Aeronautical Sciences, Toronto, Canada, ICAS Paper No. 2002-871, September, 2002.
68. Bushnell, Dennis M.: "Fluid Mechanics, Drag Reduction and Advanced Configuration Aeronautics", NASA TM-2000-210646, December, 2000
69. Pfenninger, W., and Vermuru, C. s.: "Design Aspects of Long Range Supersonic LFC Airplanes with Highly Swept Wings", SAE Paper 881397, Aerospace Technology Conference and Exposition, Anaheim, CA, October 3-6, 1988.
70. Wlezien, R., and Veitch, L.: "The DARPA Quiet Supersonic Platform Program", AIAA 2002-0311, 40th AIAA Aerospace Sciences Meeting & Exhibit, Reno, NV, Jan. 14-17, 2002
71. th AIAA Aerospace Sciences Meeting & Exhibit, Reno, NV, Jan. 14-17, 2002
72. Spalart, P. R. and Jou, W-H., and Strelets, M. and Allmaras, S. R.: "Comments on the Feasibility of LES for Wings, and on a Hybrid RANS/LES Approach," Advances in DNS/LES, Proceedings of the First AFOSR International Conference on DNS/LES, Eds. Chaoqun Liu and Zhining Liu, Greyden Press, August, 1997.
73. Vos, J. B. Rizzi, A. Darracq, D. and Hirschel, E. H.: Navier-Stokes Solvers in European Aircraft Design, Progress in Aerospace Sciences, 38, pp. 601-697, 2002.
74. Spalart, P. R.: "Strategies for Turbulence Modeling and Simulations," 4th International Symp. on Engineering Turbulence Modelling and Measurements, eds. W. Rodi and D. Laurence, Elsevier, May, 1999.
75. Hedges, L., Travin, A., and Spalart, P. R.: "Detached-Eddy Simulations Over a Simplified Landing Gear," J. Fluids Eng. 224, June, 2002.
76. nd Fluid Dynamics Conference and Exhibit, June, 2002.
77. Batten, P., Goldberg, U. and Chakravarthy, S., "Sub-Grid Turbulence Modeling for Unsteady Flow with Acoustic Resonance," AIAA Paper No. 2000-0473, 2000.
78. Zhang, H. L., Bachman, C. R., and Fasel, H. F.: "Application of a New Methodology for Simulations of Complex Turbulent Flows," AIAA Paper No. 2000-2535, 2000.
79. Girimaji, S. S., Sreenivasan, R., and Jeong, E.: "Pans Turbulence Model For Seamless Transition Between RANS LES: Fixed-Point Analysis And Preliminary Results," FEDSM2003-45336, Proceedings of ASME FEDSM'03, 4-th ASME-JSME Joint Fluids Engineering Conferences, Honolulu, Hawaii, July 13-16, 2003.
80. st Aerospace Sciences Meeting and Exhibit, Jan. 2003.
81. rd International Council on the Aeronautical Sciences, Toronto, June, 2002.
82. Chen, H., Succi, S., and Orszag, S., "Analysis of Subgrid Scale Turbulence Using the Boltzmann Bhatnagar-Gross-Krook Kinetic Equation," Physical Review E, 59, No. 3, March, 1999.
83. Carpenter, M. H., Singer, B. A., Yamaleev, N., Vatsa, V. N., Viken, S. A., and Atkins, H. L., "The Current Status of Unsteady CFD Approaches for Aerodynamic Flow Control," AIAA Paper No. 2002-3346, 2002.
84. Hardin, J.C., Ristorcelli, J. R., and Tam, C. K. W., eds., ICASE/LaRC Workshop on Benchmark Problems in Computational Aeroacoustics, NASA CP 3300, May, 1995.
85. Tam, C. K. W. and Hardin, J. C., eds., Second Computational Aeroacoustics (CAA) Workshop on Benchmark Problems, NASA CP 3352, June, 1997.
86. Dahl, M. D., ed. Third Computational Aeroacoustics (CAA) Workshop on Benchmark Problems, NASA CP-2000-209790, August, 2000.
87. Singer, B. A. and Guo, Y., Development of CAA Tools for Airframe Noise Calculations, accepted for publication in Intl. J. of Comp. Fluid Dyn., 2003.
88. nd AIAA/CEAS Aeroacoustics Conference, May, 1996.
89. th AIAA/CEAS Aeroacoustics Conference, May, 1999.
90. Batten, P., Goldberg, U. and Chakravarthy, S., "Reconstructed Sub-Grid Methods for Acoustics Predictions at all Reynolds Numbers," AIAA Paper 2002-2511, 8th AIAA/CEAS Aeroacoustics Conference & Exhibit, 2002.
91. Hunter, Craig A. and Thomas, Russell H.,"Development of a Jet Noise Prediction Method for Installed Jet Configurations", AIAA Paper No. 2003-3169, 9th AIAA/CEAS Aeroacoustics Conference & Exhibit, 2002.
92. Thilmany, J., "Probabilistic Problem Solving," Mechanical Engineering, Jan., 2002.
93. Levy, D. W., Zickuhr, T., Vassberg, J., Agrawal, S., Wahls, R. A., Pirzadeh, S., and Hemsch, M. J., "Data From the First AIAA CFD Drag Prediction Workshop," AIAA Paper No. 2002-0841, 40th AIAA Aerospace Sciences Meeting and Exhibit, January 14-17, 2002.
94. Nielsen, E. J., Lu, J., Park, M. A. and Darmofal, D. A.: "An Exact Dual Adjoint Solution Method for Turbulent Flows on Unstructured Grids," AIAA Paper No. 2003-0272, 41st AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, January 6-9, 2003
95. Alexandrov, N. M. and Lewis, R. N.: "An Overview of First Order Model Management for Engineering," Optimization and Engineering, Vol. 2, No. 4, Dec. 2001, pp. 413-430.
96. Levy, D. W., Zickuhr, T., Vassberg, J., Agrawal, S., Wahls, R. A., Pirzadeh, S., and Hemsch, M. J., Data From the First AIAA CFD Drag Prediction Workshop, AIAA Paper No. 2002-0841, 40th AIAA Aerospace Sciences Meeting and Exhibit, January 14-17, 2002
97. Venditti, D. A. and Darmofal, D. L., "Adjoint Error Estimation and Grid Adaptation for Functional Outputs: Application to Quasi-One-Dimensional Flow," Journal of Computational Physics, 164, pp. 204-227, 2000.
98. Park, M. A., "Adjoint-Based, Three-Dimensional Error Prediction and Grid Adaptation," AIAA 2002-3286, August, 2002.
99. Cruz-Neira, C., Sandin, D. J., DeFanti, T. A., Kenyon, R. V., and Hart, J. C., The CAVE: Audio Visual Experience Automatic Virtual Environment, Communications of the ACM, Volume 35, Issue 6, June 1992, ACM Press, New York, NY, USA, pp. 64-72.
100. Banks, D. C. and Kelley, M., Tracking a Turbulent Spot in an Immersive Environment. Proceedings of the 1995 ACM Symposium on Interactive 3D Graphics, ACM Press, pp. 171-172, 1995.
101. G. D. Doolen, ed., Lattice Gas Methods for Partial Differential Equations (Addison-Wesley, New York, 1990).
102. L.-S. Luo, The future of lattice-gas and lattice Boltzmann methods, in ComputationalAerosciences in the 21st Century, M. D. Salas and W. K. Anderson, eds. (Kluwer, Dordrecht, 2000), pp. 165-187
103. D. H. Rothman and S. Zaleski, Lattice-Gas Cellular Automata: Simple Models of Complex Hydrodynamics (Cambridge University Press, Cambridge, 1997).
104. Lockard, D. P., Luo, L-S, Milder, S. D., and Singer, B. A.: "Evaluation of PowerFLOW for Aerodynamic Applications," Journal of Statistical Physics, Vol. 107, Nos. 1/2, April 2002.
105. Shock, R. A., Mallick, S., Chen, H., Yakhot, V., and Zhang, R., "Recent Results on Two-Dimensional Airfoils Using a Lattice Boltzmann-Based Algorithm," Journal of Aircraft, Vol. 39, No. 3, May-June 2002.