Fortran program utilizing panel method on arbitrary lifting airfoil in two-dimensional incompressible flow to obtain Cl, Cd & Cm / Abdul Rahman Abdullah
The surfaces that support an aircraft by means of dynamic reaction on the air are called wings. Regardless of the type of lifting surface, its aerodynamic characteristics of the wing section will strongly affected by the shape of the wing section (called airfoil). The wing characteristics may be pre...
| Main Author: | |
|---|---|
| Format: | Student Project |
| Language: | English |
| Published: |
Faculty of Mechanical Engineering
1999
|
| Subjects: | |
| Online Access: | http://ir.uitm.edu.my/id/eprint/25908/ http://ir.uitm.edu.my/id/eprint/25908/1/PPd_ABDUL%20RAHMAN%20ABDULLAH%20EM%2000_5.pdf |