Semi-empirical prediction of vortex onset & progression on 65° delta wings (RTO-AVT-113, VFE-2 Facet)

46th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2008, Pages

  Nangia, R K ^a  

^a Nangia Aero Research Associates   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

CARLSON; DELTA WINGS; EXPERIMENTAL DATA; LEADING EDGE; SEMI-EMPIRICAL; TASK GROUPS; VORTICAL FLOWS;

AEROSPACE ENGINEERING; NASA; REYNOLDS NUMBER;

DELTA WING AIRCRAFT;

EID: 78149432595     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (18)

1. NANGIA, R.K. & MILLER, A.S. "Vortex Flow Dilemmas & Control on Wing Planforms for High Speeds", RTO-AVT Symposium "Advanced Flow Management, Vortex Flows & High Angle of Attack", Loen, Norway, May 2001, Meeting Proceedings RTO-MP-069 (I), SYA 9-1 to 9-14, 2003.
2. AVT-080 Report. Published by RTO & Springer Verlag, 2007.
3. NANGIA, R.K. "Applying Vortex Breakdown Empiricisms to Predict Aerodynamic Characteristics in Symmetric & Asymmetric Situations", AIAA Paper 2003-3945, 2003.
4. LUCKRING, J.M., "Reynolds Number and Leading-Edge Bluntness Effects on a 65° Delta Wing, AIAA Paper 2002-0419, 2002.
5. LUCKRING, J.M., "Transonic Reynolds Number and Leading-Edge Bluntness Effects on a 65° Delta Wing, AIAA Paper 2003-0753, 2003.
6. LUCKRING, J.M., "Compressibilty and Leading-Edge Bluntness Effects for a 65° Delta Wing, AIAA Paper 2004-0765, 2004.
7. LAMAR, J.E., "Some Recent Applications of the Suction analogy to Vortex-Lift Estimates", NASA-TM-X-72785, 1972.
8. LAMAR, J.E. & CAMPBELL. J.F., "Recent Studies at NASA Langley of Vortical Flows with Neighbouring Surfaces", AGARD-CP-342, 10-1 to 10-27, 1983.
9. CARLSON, H. W. & MACK, R.J., "Studies of Leading-Edge Thrust Phenomena", J. Aircraft., Vol. 17, No. 12, pp. 890-897, 1980.
10. CARLSON, H.W. & SHROUT, B.L. & DARDEN, C.M., "Wing Design with Attainable Leading-Edge Thrust Considerations", J. Aircraft, Vol.22, No.3, pp. 244-248, 1985.
11. POLHAMUS, E.C., "Predictions of Vortex-Lift Characteristics by a Leading-Edge Suction Analogy", J. Aircraft., Vol.8, No. 4, pp.193-199, 1971.
12. POLHAMUS, E.C., "Charts for Predicting the Subsonic Vortex-lift Characteristics of Arrow, Delta, and Diamond Wings". NASA TN-D-6243, April 1971.
13. LAN, C.E. & HSU, C.H., "Effects of Vortex Breakdown on Longitudinal and Lateral Aerodynamics of Slender Wings by the Suction Analogy", AIAA Paper 82-1385, 1982.
14. LAN, C.E., "Theoretical Prediction of Wing Rocking", AGARD CP-386, pp. 32-1 to 32-13, 1985.
15. TSENG, J.B. & LAN, C.E., "Calculation of Aerodynamic Characteristics of Airplane Configurations at High Angle of Attack", NASA CR-4182, 1988.
16. KUCHEMANN, D., The Aerodynamic Design of aircraft", Pergamon Press, Oxford, 1978.
17. NANGIA, R.K., "The Design of Manoeuvrable Wings using Panel Methods, Attained Thrust & Euler Codes", ICAS-92, China, 1992.
18. NANGIA, R.K., PALMER, M.E., "A Comparative Study of Four UCAV Wing Layouts - High-Speed Aero Performance & Stability Considerations", ICAS -2006-1.7, Germany, September 2006.