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- W2317356436 abstract "The United States Army helicopter fleet is experiencing deformation of rotor blade contours from sand erosion and the implementation of technologies to reduce it. An investigation was performed to determine the effect of these types of degradations on the tail rotor performance of Apache attack helicopters. Computational fluid dynamics was used to calculate aerodynamic coefficients for representative deformed airfoil sections. A hover analysis code was used to evaluate the impact of the damaged airfoils on the tail rotor performance. The results show that airfoil erosion can lead to a significant reduction in the maximum thrust available from worn tail rotors." @default.
- W2317356436 created "2016-06-24" @default.
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- W2317356436 date "2006-06-05" @default.
- W2317356436 modified "2023-10-05" @default.
- W2317356436 title "Blade Contour Deformation and Helicopter Performance" @default.
- W2317356436 cites W1977294541 @default.
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- W2317356436 doi "https://doi.org/10.2514/6.2006-3167" @default.
- W2317356436 hasPublicationYear "2006" @default.
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