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LoginIs pressure coefficient distributions are calculated for flow over an airfoil?
(a) True
(b) False
I have been asked this question during an online exam.
My enquiry is from Modern Low Speed Airfoils in division Incompressible Flow over Airfoils of Aerodynamics
Aerodynamics Incompressible Flow over Airfoils in Aerodynamics 3 years ago
The correct choice is (a) True
The best I can EXPLAIN: The unstructured MESH for the numerical calculation of the flow over an airfoil to calculate for pressure COEFFICIENT distributions, airfoil shapes that support the specified pressure distribution is obtained, as given by the circle. The initial airfoil shape is ALSO shown in constant scale.
Posted on 02 Dec 2021, this text provides information on Aerodynamics related to Incompressible Flow over Airfoils in Aerodynamics. Please note that while accuracy is prioritized, the data presented might not be entirely correct or up-to-date. This information is offered for general knowledge and informational purposes only, and should not be considered as a substitute for professional advice.
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