Speculation of local aerodynamic loads on helicopter rotor blade in forward flight
Dayhoum, A., Zakaria, M., Elshabka, A., Abdelhamid, O. (2019). Speculation of local aerodynamic loads on helicopter rotor blade in forward flight. EKB Journal Management System, 18(18), 1-9. doi: 10.1088/1757-899X/610/1/012099
Abdallah Dayhoum; Mohamed Y. Zakaria; A. M. Elshabka; O. E. Abdelhamid. "Speculation of local aerodynamic loads on helicopter rotor blade in forward flight". EKB Journal Management System, 18, 18, 2019, 1-9. doi: 10.1088/1757-899X/610/1/012099
Dayhoum, A., Zakaria, M., Elshabka, A., Abdelhamid, O. (2019). 'Speculation of local aerodynamic loads on helicopter rotor blade in forward flight', EKB Journal Management System, 18(18), pp. 1-9. doi: 10.1088/1757-899X/610/1/012099
Dayhoum, A., Zakaria, M., Elshabka, A., Abdelhamid, O. Speculation of local aerodynamic loads on helicopter rotor blade in forward flight. EKB Journal Management System, 2019; 18(18): 1-9. doi: 10.1088/1757-899X/610/1/012099

Speculation of local aerodynamic loads on helicopter rotor blade in forward flight

International Conference on Aerospace Sciences and Aviation Technology
Article 100, Volume 18, Issue 18, April 2019, Page 1-9  XML PDF (1.5 MB)
Document Type: Original Article
DOI: 10.1088/1757-899X/610/1/012099
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Authors
Abdallah Dayhoum1; Mohamed Y. Zakaria2; A. M. Elshabka3; O. E. Abdelhamid4
1MSc. Student, Military Technical College, Aerospace Engineering Department, 11766 Cairo, EGYPT.
2Assistant Professor, Acting as department head, Military Technical College, Aerospace Engineering Department, 11766 Cairo, EGYPT.
3Assistant Professor, Military Technical College, Aerospace Engineering Department, 11766 Cairo, EGYPT.
4Professor, Military Technical College, Aerospace Engineering Department, 11766 Cairo, EGYPT.
Abstract
Design of rotor blade is mainly the most important consideration in helicopter industry. A sufficient input data is needed for various flight conditions that should be accounted for in rotor design process. In this paper, blade element theory is applied to helicopter rotor blade in forward flight. The main objective is to assure the fidelity of using blade element theory in helicopter rotor blade design. Blade element theory is used for calculating the average lift, thrust, power for rotary wings and the local aerodynamic loads. The local non-dimensional normal force coefficients obtained from blade element theory were compared with experimental results of the 7A rotor at five non dimensional radial positions for the high speed test point 312. The results showed the same pattern of variation along the azimuth with a considered convergence along the blade radius.
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