INVESTIGATION AND MODIFICATION OF AERODYNAMIC CHARACTERISTICS OF SUPERSONIC AIRCRAFT
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Abstract
Increasing the aerodynamic efficiency and enhancing the supermaneuverability for the selected supersonic aircraft (F-16A) is presented. Aerodynamic characteristics, surface pressure distribution and maximum lift are are estimated for the baseline configuration for different Mach number and angles of attack in subsonic and supersonic potential flow, using a low order three- dimensional panel method supported with semi-empirical formulas of Datcom.
Estimation of the total nose-up and nose-down pitching moments about the center of gravity of the completed aircraft in subsonic region depending on the flight conditions and aircraft performance limitations. A modern program was implemented by suggesting a two dimensional thrust vectoring technique (pitch vectoring up and down) controlled by the best design of advanced aerodynamic and control surface (foreplane or canard). Work results shows that the canard (as a control surface) with thrust vectoring produces enough nose-down moment and can support the stabilator at high maneuvers, while for an aerodynamic surface, a rate of (5-6%) increase was achieved in the aerodynamic efficiency (lift-to-drag ratio) of the baseline configuration in both subsonic and supersonic flight
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References
AIRCRAFT Cy-20, Technical Description, BOOK 1, "GENERAL INFORMATION AND FLIGHT PERFORMANCE", TOP SECRET, Copy No. 28, 1972.
B. Etkin and L. D. Reid, "Dynamics of Flights: Stability and Control", John Wiley & Sons, New York, NY, third edition, 1996.
Col. William D. Siuru, Jr., "Supermaneuverability", Aerospace Power Journal, Spring, 1988.
Email: [email protected]
Danie P. Raymer, "Aircraft Design: A Conceptual Design", AIΑΑ, 1992.
Fink, R.D., "USAF Stability and Control DATCOM", Wright-Patterson AFB, OH, 1975. "F-15 ACTIVE (Advanced Control Technology for Integrated Vehicles)- Research Program History and Technology", Document: EG-2003-01-001-DFRC, NASA Dryden Flight Research Center, 2003.
Hoak, D., Ellison, D, et al., "USAF DATCOM", Air Force Flight Dynamics Lab, Wright-Patterson AFB, OH.
John J. Bertin, Randall J. Stiles, and Steven A. Brandt, "Introduction to Aeronautics: A Design Perspective", American Institute of Aeronautics and Astronautics, January 1997.
Kotelnikov, G. N., "Airplane Aerodynamics". Textbooks for Cadets of aircraft-Technician Officer Schools, Russia, 1973.
L. Morino and CC Luo, Subsonic Potential Aerodynamics for Complex Configurations. A General Theory", AIAA Journal, Vol. 12, No. 2, February 1974
Mason, W H. "Applied Computational Aerodynamics", Internet Pages (a PDF File), April 1998
Nelson, R. C., "Flight Stability and Automatic Control", WCB McGraw-Hill, New York, NY, second edition, 1998.
Perkins, D. Courtland and Hage, E. Robert, "Airplane Performance Stability and Control", John Wiley & Sons, New York, NY, 1949
Shaker M. Hussain, "Flight Performance Optimization of Supersonic General Aviation Design", Ph.D Thesis, Military College of Engineering, Baghdad, 2000
Venik's Aviation, Breakthrough in Supermaneuverability", June 19,2002
Email: www.acronics.ru//venik.way.to