SOFTWARE DEVELOPMENT FOR AERODYNAMIC CHARACTERISTICS ESTIMATION OF WING-BODY COMBINATION OF AIRCRAFT AT SUBSONIC SPEEDS
Keywords:
KeywordsAbstract
The study of aerodynamic characteristics is an important aspects in designing of an aircraft. The
estimate of the lift and drag coefficients of the combination of wings and bodies at subsonic
speeds. The calculation of these aerodynamic characteristics is a tedious workout in the
preliminary design, as it has to be carried out repetitively for every different combination. A
software for determining the wing-body combination lift and drag coefficients known as AC
Estimator is being developed to serve as a solution to the tedious and time-consuming design
method. The development and capabilities of this software to predict varieties aerodynamic
characteristics with good accuracy as compared to manual calculation are being presented and
discussed in this paper.
References
D.E.Hoak, R.D.Finck , et al, 1978, USAF Stability and Control Datcom Flight Control Division, Air Force Flight Dynamics Laboratory, Wright Patterson Air Force Base, Ohio.
Dr. Jan Roskam, 1990, Airplane Design Part IV : Preliminary Calculation of Aerodynamic, Thrust and Power Charac teristics. Kansas : Roskam Aviation and Engineering Corporation.
The Royal Aeronautical Society, 1981, ESDU 76003 - Geometrical Properties of Cranked and Straight Tapered Wing Planform, United Kingdom : The Royal Aeronautical Society.
John D. Anderson, 1989, Introduction to Flight. Singapore : McGraw Hill International Edition.
Abbott, Ira-H . and Doenhoff, Albert-E. -Von, 1959, Theory of Wing Section,. New York: Dover Publication, Inc.
Frederick O. Smetana, 1984, Computer Assisted Analysis of Aircraft Performance Stability and Control, United State of Americ a : McGraw Hill Inc.
E L Houghton & N B Carruthers, 1982, Aerodynamics f or Engineering Student, Scotland : Edward Arnold.
Che Rahim Che The, 2000, Kaedah Berangka, Malaysia: Faculty of Science, University of Technology Malaysia.
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