Sensing aircraft icing effects by flap hinge moment measurement

17th Applied Aerodynamics Conference

Volumn , Issue , 1999, Pages 368-378

  Gurbacki, Holly M ^a   Bragg, Michael B ^a  

^a UNIVERSITY OF ILLINOIS AT URBANA CHAMPAIGN   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; DIES; FLOW SEPARATION; LIFT; WIND TUNNELS;

AERODYNAMIC COEFFICIENTS; FLAP HINGE MOMENT; FLOW CHARAC-TERISTICS; PITCHING MOMENTS; SEPARATION BUBBLE; STEADY-STATE VALUES; SUBSONIC WIND TUNNELS; SURFACE PRESSURE DISTRIBUTION;

ICE;

EID: 84873160087     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1999-3149     Document Type: Conference Paper

References (10)

1. Bragg, M.B., Perkins, W.R., Sarter, N.B., Basar, T., Voulgaris, P.G., Gurbacki, H.M., Melody, J.W., McCray, S.A., "An Interdisciplinary Approach to In-flight Aircraft Icing Safety," AIAA Paper 98-0095, Reno, NV, 1998.
2. Trunov, O.K. and Ingelman-Sundberg, M., "On the Problem of Horizontal Tail Stall Due to Ice," The Swedish-Soviet Working Group on Scientific-Technical Cooperation in the Field of Flight Safety, Report No. JR- 3, 1985.
3. Johnson, C.L., "Wing Loading, Icing and Associated Aspects of Modern Transport Design," Journal of the Aeronautical Sciences, vol. 8, no. 2, December 1940, pp. 43-54.
4. Bragg, M.B., "Aircraft Aerodynamic Effects due to Large Droplet Ice Accretions," AIAA Paper 96-0932, Reno, NV, 1996.
5. Pruzan, D.A., Khatkhate, A.A., Gerardi, J.J., Hickman, G.A., "Smart Skin Technology Development for Measuring Ice Accretion, Stall, and High AOA Aircraft Performance, Final Technical Report, Part 2, Surface Pressure Separation/Stall Detector Development," NASA Contract No. NAS3-25966, Report No. 93D-03-0423, April 23, 1993.
6. Maris, J.M., "Airfoil Performance Monitoring using the Turbulence Intensity Parameter," Proceedings of the FAA International Conference on Aircraft In-flight Icing, Vol. II, Working Group Papers, Final Report, August, 1996.
7. Cronin, D., Vogel, J., and Lamb, M., "Analytical Development and Experimental Results of a Method for Aerodynamic Contamination Detection," International Icing Symposium’95, September 18-21, 1995.
8. Rae, W. H. and Pope, A., Low-Speed Wind Tunnel Testing, John Wiley & Sons, 1984.
9. Althaus, D. and Wortmann, F. "Experimental Results from the Laminar Wind Tunnel of the Institute for Aerodynamic and Gasdynamics - The University of Stuttgart" published by Princeton University, Department of Mechanical and Aerospace Engineering, 1979.
10. Lee, S., Dunn, T., Gurbacki, H. M., Bragg, M. B, Loth, E., "An Experimental and Computational Investigation of Spanwise-Step-Ice Shapes on Airfoil Aerodynamics", AIAA 98-0490, January, 1998.