A free-wake, lifting-surface model using distributed vorticity elements

Collection of Technical Papers - AIAA Applied Aerodynamics Conference

Volumn 1, Issue , 2004, Pages 635-645

  Bramesfeld, Götz ^a,c   Maughmer, Mark D ^a,c   Horstmann, Karl Heinz ^b,c  

^a PENNSYLVANIA STATE UNIVERSITY   (United States)

^b GERMAN AEROSPACE CENTER DLR   (Germany)

^c 233 Hammond Bldg ^*

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT MODELS; DRAG; LIFT; NUMERICAL METHODS; POTENTIAL FLOW; WINGS;

DOWNWASH; INTEGRATED SPANWISE CIRCULATION; PANEL METHODS; VORTICITY;

WAKES;

EID: 20744448670     PISSN: 10485953     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2004-5075     Document Type: Conference Paper

References (10)

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2. Eppler, R., "Induced Drag and Winglets," Aerospace Science and Technology, No. 1, 1997, pp. 3-15.
3. Mortara, K.W. and Maughmer, M.D., "A Method for the Prediction of Induced Drag for Planar and Non-Planar Wings," AIAA 93-3420-CP, August 1993.
4. Schmidt-Göller, S., "Zur genauen Berechnung des induzierten Widerstands von Tragflügeln," Doctoral Thesis, Universität Stuttgart, Stuttgart, Germany, 1992.
5. Munk, M., "The Minimum Induced Drag Aerofoils,", NACA Report No. 121, 1921.
6. Katz, J. and Plotkin, A., Low-Speed Aerodynamics, McGraw-Hill, New York, 1991.
7. Bippes, H., "Experimente zur Entwicklung der freien Wirbel hinter einem Rechteckflügel," Acta Mechanica 26, Springer Verlag, 1977, pp. 223-245.
8. Van Dyke, M. (Editor), Album of Fluid Motion, Parabolic Press, Stanford, 1982.
9. Smith, S., Kroo, I., "computation of Induced Darg for Elliptical and Crescent-Shaped Wings," Journal of Aircraft, Vol. 30, No. 4, July-Aug. 1993, pp. 446-452.
10. Leyser, J., "Accurate Computation of Lift and Induced Drag at Lifting Surfaces," AIAA 96-2405-CP, 1996.