Aerodynamics of a finite wing with simulated ice
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[1] Tuncer Cebeci,et al. Effects of enviromentally imposed roughness on airfoil performance , 1987 .
[2] Beverly G Gulick. Effects of a Simulated Ice Formation on the Aerodynamic Characteristics of an Airfoil , 1938 .
[3] W. D. Harvey,et al. Juncture flow control using leading-edge fillets , 1985 .
[4] Brian M. Berkowitz,et al. An experimental investigation of multi-element airfoil ice accretion and resulting performance degradation , 1989 .
[5] William H. Rae,et al. Low-Speed Wind Tunnel Testing - second edition , 1984 .
[6] M. Kerho,et al. Neutrally buoyant bubbles used as flow tracers in air , 1993 .
[7] R. W. Hale,et al. Development of an Integrated System for Flow Visualization in Air Using Neutrally-Buoyant Rubbles , 1971 .
[8] O K Trunov,et al. METHODS FOR PREDICTION OF THE INFLUENCE OF ICE ON AIRCRAFT FLYING CHARACTERISTICS , 1977 .
[9] William J. Devenport,et al. Turbulence structure near the nose of a wing-body junction , 1987 .
[10] M. B. Bragg,et al. Measured aerodynamic performance of a swept wing with a simulated ice accretion , 1990 .
[11] Tuncer Cebeci,et al. Calculation of Flow Over Iced Airfoils , 1988 .
[12] Michael B. Bragg,et al. LDV flowfield measurements on a straight and swept wing with a simulated ice accretion , 1993 .
[13] W. D. Harvey,et al. Flow control in a wing/fuselage-type juncture , 1988 .
[14] Michael B. Bragg. An experimental study of the aerodynamics of a NACA0012 airfoil with a simulated glaze ice accretion, volume 2 , 1986 .
[15] M. B. Bragg,et al. Aerodynamic measurements of an airfoil with simulated glaze ice , 1986 .
[16] Abdollah Khodadoust,et al. An Experimental Study of the Flowfield on a Semispan Rectangular Wing With a Simulated Glaze Ice Accretion , 1994 .
[17] Oh Joon Kwon,et al. Simulation of iced wing aerodynamics , 1991 .
[18] Michael B. Bragg,et al. Effect of a simulated ice accretion on the aerodynamics of a swept wing , 1991 .
[19] W. Roger Briley,et al. Numerical prediction of incompressible separation bubbles , 1975, Journal of Fluid Mechanics.
[20] Robert J. Mcghee,et al. Evaluation of tunnel sidewall boundary-layer-control systems for high-lift airfoil testing , 1991 .
[21] Robert P. Cassoni,et al. Aircraft Anti-Icing and De-Icing Techniques and Modeling , 1996 .
[22] G. Gregorek,et al. Airfoil aerodynamics in icing conditions , 1986 .
[23] I. Tani. Low-speed flows involving bubble separations , 1964 .
[24] F. Gessner,et al. Experimental Investigation of Flow About a Strut-Endwall Configuration , 1990 .
[25] M. B. Bragg,et al. Experimental measurements in a large separation bubble due to a simulated glaze ice shape , 1988 .
[26] H. Bippes,et al. Half Model Testing Applied to Wings above and below Stall , 1982 .
[27] S. Hoerner. Fluid-Dynamic Lift , 1985 .
[28] M. B. Bragg,et al. Measurements in a leading-edge separation bubble due to a simulated airfoil ice accretion , 1992 .
[29] Michael B. Bragg,et al. Effect of simulated glaze ice on a rectangular wing , 1989 .
[30] Lakshmi N. Sankar,et al. Numerical study of the effects of icing on finite wing aerodynamics , 1990 .
[31] Michael B. Bragg. Experimental aerodynamic characteristics of an NACA 0012 airfoil with simulated glaze ice , 1988 .
[32] Mark Potapczuk. Numerical analysis of a NACA0012 airfoil with leading edge ice accretions , 1988 .
[33] Lakshmi N. Sankar,et al. Numerical investigation of performance degradation of wings and rotors due to icing , 1992 .