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Analyzing a NACA 23012 Airfoil Composed of a Double-Slotted Fowler Flap and a Leading-Edge Handley-Page Slat with the Use of Computational Fluid Dynamics
Technical Paper
2006-01-2385
ISSN: 0148-7191, e-ISSN: 2688-3627
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English
Abstract
Today, Computational Fluid Dynamics (CFD) is more commonly used in aerospace industry, and becoming an essential engineering tool. CFD is largely being used as a preliminary design tool, and often accompanied by wind tunnel test for modeling validation. Embry-Riddle Aeronautical University (ERAU), Prescott campus, one of the few universities in the U.S. to provide strong undergraduate hands-on CFD curriculum, allowed a group of students the opportunity to model flow over two different airfoils using CFD applications and also with the use of a subsonic wind tunnel for CFD validations. A NACA 23012 airfoil with a double slotted Fowler flap and a leading edge Handley-Page slat was created for the purpose of this analysis. This research effort is an example of using both structured and unstructured grid CFD to expose students at an undergraduate level and to recognize its relationship between experimental data on an aircraft wing design.
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Citation
Glaser, A. and Hayashibara, S., "Analyzing a NACA 23012 Airfoil Composed of a Double-Slotted Fowler Flap and a Leading-Edge Handley-Page Slat with the Use of Computational Fluid Dynamics," SAE Technical Paper 2006-01-2385, 2006, https://doi.org/10.4271/2006-01-2385.Also In
References
- American Institute of Aeronautics and Astronautics, Inc. 1997 Re-Engineering the Design Process through Computation Jameson, A.
- American Institute of Aeronautics and Astronautics, Inc. 1998 Investigation of Confluent Boundary Layers In High-Lift Flows Ying, S. X. Spaid, F. W. McGinley, C. B. Rumsey, C. L.
- Lynch, F.T. Potter, R. C. Spaid, F. W. 1996 Requirements for Effective High Lift CFD ICAS Proceedings, 20 th Congress
- Anderson, J.D. 2005 Introduction To Flight Boston Mc-Graw Hill
- Abbott, I. Von Doenhoff, A. 1959 Theory of Wing Sections New York Dover Publications, Inc.
- Helio Phaeton Aerospace 2005 AE 420 Aircraft Preliminary Design Phase IV Report Unpublished technical report, College of Engineering Prescott, AZ Embry-Riddle Aeronautical University
- Helio Phaeton Aerospace 2006 AE 421 Aircraft Detail Design Midterm Report Unpublished technical report, College of Engineering Prescott, AZ Embry-Riddle Aeronautical University
- American Institute of Aeronautics and Astronautics, Inc. 1999 Aerodynamic Performance of an Innovative Flap Design Papadakis, M. Wong, S. Yeong, H.
- American Institute of Aeronautics and Astronautics, Inc. 2000 Realization of a Shapevariable Fowler Flap for Transport Aircraft Anhalt, C. Breitbach, E. Sachau, D.
- American Institute of Aeronautics and Astronautics, Inc. 1965 Aerodynamic Design Philosophy of the Boeing 737 Olason, M. L. Norton, D. A.
- Barlow, J. B. Rae, W. Pope, A. 1999 Low-Speed Wind Tunnel Testing New York John Wiley & Sons, Inc.