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Predicting Aircraft Performance Degradation Due to Ice Accretion
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English
Abstract
An analytical method to predict the performance degradation of aircraft with ice accretion is presented. Early research on airfoil icing and the effects of ice on aircraft are reviewed. Data on the performance degradation of airfoils due to ice are presented as they apply to the aircraft performance analysis. A computer code has been written and results are discussed.
Citation
Bragg, M. and Gregorek, G., "Predicting Aircraft Performance Degradation Due to Ice Accretion," SAE Technical Paper 830742, 1983, https://doi.org/10.4271/830742.Also In
References
- Gray, Vernon H. “Prediction of Aerodynamic Penalties Caused by Ice Formations on Various Airfoils” NASA TN D-2166 1964
- Ingelman-Surdberg, M. Trunov, O.K. Ivaniko, A. “Methods for Prediction of the Influence of Ice on Aircraft Flying Characteristics” a joint report from the Swedish-Soviet Working Group on Flight Safety, 6th Meeting 1977
- Ingelman-Surdberg, M. Trunov, O.K. “Wind Tunnel Investigation of the Hazardous Tail Stall Due to Icing” Report No. JR-2, a joint report from the Swedish-Soviet Working Group on Flight Safety 1977
- Shaw, Robert J. Sotos, Ray G., “An Experimental Study of Airfoil Icing Characteristics” NASA TM 82790 1982
- Bragg, M.B. Gregorek, G.M. Shaw, R.J. “Wind Tunnel Investigation of Airfoil Performance Degradation Due to Icing” 82 12th Aerodynamic Testing Conference Williamsburg, Virginia 1982
- Bragg, M.B. Zaguli, R.J. Gregorek, G.M. “Wind Tunnel Evaluation of Airfoil Performance Using Simulated Ice Shapes” Aeronautical and Astronautical Research Laboratory, The Ohio State University, AARL TR 82-01 1982
- Bragg, M.B. Gregorek, G.M. “Aerodynamic Characteristics of Airfoils with Ice Accretions” 82 20th Aerospace Sciences Meeting Orlando, Florida 1982
- Bragg, M.B. “Rime Ice Accretion and Its Effect on Airfoil Performance,” Ph.D. Dissertation, The Ohio State University 1981 1982
- Bragg, M.B. Gregorek, G.M. Shaw, R.J. “An Analytical Approach to Airfoil Icing” 81 19th Aerospace Sciences Meeting St. Louis, Missouri 1981
- Preston, Merritt G. Blackman, Calvin C., “Effect of Ice Formations on Airplane Performance in Level Cruising Flight” NACA 1598 1948
- Leckman, Paul R., “Qualification of Light Aircraft for Flight in Icing Conditions” Society of Automotive Engineers Paper No. 710394 1971
- Dieteriberger, Mark, “Evaluation of AER0ICE” Final Report, Contract F33615-79-C-3030 1981
- Neel, C.B., Jr. Bright, L.G. “The Effect of Ice Formations on Propeller Performance” NACA TN 2212 1950
- Korkan, K.D. “Performance Degradation of Propeller/Helicopter Rotor Systems Due to Rime Ice Accretion” The Second Icing Analysis Workshop, NASA Lewis Research Center 1983
- Kepple, William L., “Determination of Aircraft Antenna Loads Produced by Natural Icing Conditions,” NACA RM E7H26A
- Dvorak, F. “CLMAX Program Description,” AMI Report 7905 1979
- Dvorak, F.A. “Calculation of Turbulent Boundary Layers on Rough Surfaces in Pressure Gradient” AIAA Journal 7 9 1969 1752 1759
- Bragg, M.B. “Airfoil Performance Degradation” NASA Lewis Research Center 1983
- Gray, Vernon H. Von Glahn, Uwe H., “Aerodynamic Effects Caused By Icing of an Unswept NACA 65A004 Airfoil” NACA TN 4155 1957
- Smentana, F.0., Summey, D.C. Smith, N.S., Carden, R.K., “Light Aircraft Lift, Drag, and Moment Prediction - A Review and Analysis” NASA CR-2523 1975
- Eppler, Richard Somers, Dan M., “A Computer Program for the Design and Analysis of Low-Speed Airfoils” NASA TM 80210 1980
- Bristow, D.R. “Development of Panel Methods of Subsonic Analysis and Design” NASA Contractor Report 3234 1980
- Norment, Hillyer G., “Three Dimensional Particle Trajectory Calculation” presented at The Second Icing Analysis Workshop, NASA Lewis Research Center 1983
- Anderson, J.D. Jr., Corda, S., Van Mie, D.M., “Numerical Lifting Line Theory Applied to Drooped Leading-Edge Wings Below and Above Stall” AIAA Journal of Aircraft 17 12 1980 898 904