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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Main Author: | Abdul Rahman Abdullah (Author) |
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Format: | Thesis Book |
Language: | English |
Published: |
Shah Alam, Selangor
UNIVERSITI TEKNOLOGI MARA. FACULTY OF MECHANICAL ENGINEERING
1999
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Subjects: | |
Online Access: | Click Here to View Status and Holdings. |
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