Wind tunnel aerodynamics in rotary tests of combat aircraft models

35th Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1997, Pages

  Ericsson, Lars E ^a   Beyers, Martin E ^b  

^a Aerodynamics Laboratory ^*  (United States)

^b NATIONAL RESEARCH COUNCIL CANADA   (Canada)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; REYNOLDS NUMBER; WIND TUNNELS;

COMBAT AIRCRAFT; HIGH REYNOLDS NUMBER; SUBSCALE TEST; VELOCITY VECTORS; WORKING GROUPS;

AERODYNAMICS;

EID: 84983126688     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (28)

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2. Ericsson, L Fu and Reding, j. P., “Dynamic simulation Through Analytic Extrapolation,” Journal of Spacecraft and Rockets, Vol. 19, № 2, 1982, pp. 160-166.
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4. Cooperative Programme on Rotary Experiments for Maneuvering Aircraft Dynamics, Report of AGARD FDP WG16, to be published, 1996.
5. Beyers, M. E and Ericsson, L E, “Ground Facility Interference on Aircraft Configurations with Separated Flow,” Journal of Aircraft, Vol. 30, № 5, 1993, pp. 682-688.
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8. Ericsson, L E and Beyers, M. E., “Special Aerodynamic Considerations,” Chapter 5, AGARD-AR-265, Dec. 1990, pp. 88-97.
9. Ericsson, L E and Reding, J. P., “Asymmetric Flow Separation and Vortex Shedding on Bodies of Revolution,” Progress in Astronautics and Aeronautics, Vol. 141, 1992, pp. 391-452.
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13. Ericsson, L E., “Moving Wall Effects in Unsteady Flow,” Journal of Aircraft, Vol. 25, No, 11, 1988, pp. 977-990.
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19. Beyers, M. E, “Consolidating Critically Contaminated Coning Characteristics,” to be published.
20. Beyers, M. E and Ericsson, L E, “Extraction of Subscale Free-Flight Aerodynamics from Rotary Tests of Combat Aircraft,” AIAA Paper 97-0730, Jan. 1997.
21. Tristrant, D. R., Gauthier, F. F., and Vanmansart, M. G., “Dynamic Tests in ONERA-MFL Lille Wind Tunnels with AGARD Generic Fighter Model,” Preliminary Report, Nov. 1994.
22. Ericsson, L E, “Unsteady Flow Separation on Slender Bodies at High Angles of Attack,” Journal of Spacecraft and Rockets, Vol. 30, № 6, 1993, pp. 689-695.
23. Beyers, M. E and Ericsson, L E, “Aerodynamic Analysis and Interpretation of WG16 Results,” Cooperative Programme on Rotary Experiments for Maneuvering Aircraft Dynamics, Report of AGARD FDP WG16, Appendix 4, to be published, 1996.
24. Brandon, J. M. and Nguyen, L T., “Experimental Study of Effects of Forebody Geometry on High Angle-of-Attack Stability,” Journal of Aircraft, Vol. 25, № 7, 1988, pp. 591-597.
25. Ericsson, L E, “Wing Rock Generated by Forebody Vortices,” Journal of Aircraft, Vol. 20, № 2, 1989, pp. 110-116.
26. Ericsson, L. E., “Further Analysis of Wing Rock Generated by Forebody Vortices.” Journal of Aircraft, Vol. 20, № 12, 1989, pp. 1089-1104.
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28. Ericsson, L. E. and Beyers, M. E., “Fluid/Motion Coupling in Conceptual Supennaneuvers,” AIAA Paper 96-0787, Jan. 1996.