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LoginNACA 0023 is______
(a) Negatively cambered airfoil
(b) Positively cambered airfoil
(c) Symmetrical airfoil
(d) Thin cambered airfoil
This question was posed to me in my homework.
The question is from The Cambered Airfoil in portion Incompressible Flow over Airfoils of Aerodynamics
Aerodynamics Incompressible Flow over Airfoils in Aerodynamics 3 years ago
To explain: The first two digits in the NACA nomenclature give the maximum camber and POSITION of maximum camber. For a symmetric airfoil, both of these are zero.
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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