THEORETICAL AND EXPERIMENTAL INVESTIGATION OF SOME LATERAL CONTROL DERIVATIVES OF RECTANGULAR. WING
El-Sharnoby, M., Metwally, M., Abdel-Hamid, O. (1997). THEORETICAL AND EXPERIMENTAL INVESTIGATION OF SOME LATERAL CONTROL DERIVATIVES OF RECTANGULAR. WING. EKB Journal Management System, 7(ASAT Conf. 13-15 May 1997), 53-66. doi: 10.21608/asat.1997.25389
M. El-Sharnoby; Metwally H. Metwally; O E. Abdel-Hamid. "THEORETICAL AND EXPERIMENTAL INVESTIGATION OF SOME LATERAL CONTROL DERIVATIVES OF RECTANGULAR. WING". EKB Journal Management System, 7, ASAT Conf. 13-15 May 1997, 1997, 53-66. doi: 10.21608/asat.1997.25389
El-Sharnoby, M., Metwally, M., Abdel-Hamid, O. (1997). 'THEORETICAL AND EXPERIMENTAL INVESTIGATION OF SOME LATERAL CONTROL DERIVATIVES OF RECTANGULAR. WING', EKB Journal Management System, 7(ASAT Conf. 13-15 May 1997), pp. 53-66. doi: 10.21608/asat.1997.25389
El-Sharnoby, M., Metwally, M., Abdel-Hamid, O. THEORETICAL AND EXPERIMENTAL INVESTIGATION OF SOME LATERAL CONTROL DERIVATIVES OF RECTANGULAR. WING. EKB Journal Management System, 1997; 7(ASAT Conf. 13-15 May 1997): 53-66. doi: 10.21608/asat.1997.25389

THEORETICAL AND EXPERIMENTAL INVESTIGATION OF SOME LATERAL CONTROL DERIVATIVES OF RECTANGULAR. WING

International Conference on Aerospace Sciences and Aviation Technology
Article 5, Volume 7, ASAT Conf. 13-15 May 1997, May 1997, Page 53-66  XML PDF (2.77 MB)
Document Type: Original Article
DOI: 10.21608/asat.1997.25389
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Authors
M. El-Sharnoby1; Metwally H. Metwally2; O E. Abdel-Hamid3
1Associate professor, Benha High Technology Institute, Benha, Egypt.
2Faculty member, Military Technical College, Cairo, Egypt.
3Prof. of Aerod) riar•ics, Military Technical College, Cairo, Egypt.
Abstract
In the field of Appred Aerodynamics, the evaluation of aerodynamic derivatives is essential for analysis of stability and control of flying bodies. In the present work some of important stability and control derivatives are calculated theoretically for a rectangular wing in an incompressible flow The theoretical solution is realized on the basis of two different methods; the Multhopp's method and the Von& Lattice Method (VLM). An experimental evaluation of the calculated derivatives is also performed. The experimental study was carried out by the testing of a wing model in a general-purpose low speed wind tunnel. A good agreement was found between theoretical and experimental results.
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