Lift coefficient predictions for delta wing under pitching motions

32nd AIAA Fluid Dynamics Conference and Exhibit

Volumn , Issue , 2002, Pages

  Jouannet, Christopher ^a   Krus, Petter ^a  

^a LINKÖPING UNIVERSITY   (Sweden)

Author keywords

[No Author keywords available]

Indexed keywords

DELTA WINGS; DYNAMIC EFFECTS; LIFT COEFFICIENT; PITCHING MOTION; PREDICTION METHODS; PRELIMINARY DESIGN;

DELTA WING AIRCRAFT; FLUID DYNAMICS;

LIFT;

EID: 84896694110     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (14)

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2. Traub L. W.,"Prediction of Vortex Breakdown and Longitudinal Characteristics of Swept Slender Planforms," Journal of Aircraft, Vol. 34, No 3, May-June 1997
3. Erickson Gary E.,"Flow Studies of Slender Wing Vortices," AIAA-80-1423
4. Lawford J. A. & Beauchamp A. R., "Low-Speed Wind-Tunnel Measurements on a Thin Sharp-Edged Delta Wing with 70° Leading Edge Sweep, with Particular Reference to the Position of Leading-Edge-Vortex Breakdown," ARC 3338, 1963.
5. Goman M. and Khrabov A.,"State-Space Representation of Aerodynamic Characteristics of an Aircraft at High Angles of Attack," Journal of Aircraft, Vol. 31, No.5, Sept.-Oct. 1994
6. Jones, R. T., "Properties of Low Aspect Ratio Wings at Speeds Below and Above the Speed of Sound," NACA Rept. 835, 1946, pp 59-63
7. Pelletier, A. & Nelson, R. C., "An Experimental Study of Static and Dynamic Vortex Breakdown on Slender Delta Wing Planforms," AIAA-94-1879-CP, 1994.
8. Ericsson, L. E., "Vortex Breakdown Dynamics on Pitching Delta Wings," AIAA-95-1777-CP, 1995
9. Barlow, J. B. & Rae, W. H., Jr & Pope, A., "Low-Speed Wind Tunnel Testin" Third Edition, Wiley Interscience ISBN 0-471-55774-9, 1999.
10. Jouannet, Ch., "A Water Tunnel Study of Vortical Flows over Delta Wings," Linköpings Universitet, LiTH-IKP-EX-1786, 2001
11. Wentz, W. H., Jr & Kohlman D. L., "Wind Tunnel Investigation of Vortex Breakdown on Slender Sharp-Edged Wings," NASA Research Grant NGR-17-002-043, 1968
12. Earnshaw, P. B., Lawford, J. A., "Low-Speed Wind-Tunnel Experiment on a Series of Sharp-Edged Delta Wings," ARC 3424, 1966
13. Soltani, M. R. & Bragg, M. B. & Brandon, J. M.,"Experimental Measurement on an Oscillating 70-degree Delta Wing in Subsonic Flow," AIAA-88-2576-CP, 1998
14. Goman, M. G., Greenwell, D. I., Khrabov A.N., "The Characteristic Time Constant Approach for Mathematical Modelling of High Angle of Attack Aerodynamics" ICAS 2000 Congress.