FORTRAN PROGRAM UTILIZING PANEL METHOD ON ARBITRARY LIFTING AIRFOIL IN TWO DIMENSIONAL INCOMPRESSIBLE FLOW TO OBTAIN C1, Cd & Cm

FORTRAN PROGRAM UTILIZING PANEL METHOD ON ARBITRARY LIFTING AIRFOIL IN TWO DIMENSIONAL INCOMPRESSIBLE FLOW TO OBTAIN C1, Cd & Cm

The surface that support an aircraft by menas of dynamics reactions on the air are called wings. Regardlessof the type of lifting surface, its aerodynamics characteristics of the wing section will strongly affected by the shape of the wing section.

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Bibliographic Details
Main Author: Abdul Rahman Abdullah (Author)
Format: Thesis Book
Language:English
Published: Shah Alam, Selangor UNIVERSITI TEKNOLOGI MARA. FACULTY OF MECHANICAL ENGINEERING 1999
Subjects:
Aerofoils > Testing
Aerofoils
Air flow
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