Hybridlete wrote:
Ai_1 wrote:
Please explain the use of the term fuselage and the inclusion of a circular cross sectional image on the sketch if this is not for cylindrical bodies. I think you'll find my interpretation is correct but I'd be happy to be corrected if I am in fact wrong.
The circle in the images are so that you can see the airfoils line up and provide a point of reference, not because this is for cylinders.
SMH. I don't even know how you could even think that. What is the point of the tear drop and Kamm Tail shape outlines then?
And the values given are Cd numbers, meaning it is valid for other uses, not just aircraft fuselages. Do you even realize that virtually all the airfoils used in the bike industry come from the NCAA testing done for aircraft?
For starters, it's NACA, not NCAA.
And yes, I'm very familiar with NACA airfoils. More so than yourself I dare say. Most of them are rather old by the way, from the first few decades of aviation. There are better airfoils for most applications but NACA airfoils are still a common point of reference and are still useful for non-critical applications. Anyway, NACA airfoils seem a little off topic here, in what's already an off topic discussion, so back to the issue at hand...
Apologies if my use of the word cylindrical caused any confusion, perhaps if I used engineering terminology and called them surfaces of revolution you'd understand what I mean?
As I said earlier, your comments thus far lead me to believe you consider this subject to be simpler than it is. It's a commonly understood phenomenon that incompetence breeds confidence and overestimation of ones own ability. I think that's at play here (Refer to the Dunning Kruger Effect).
Airflows are complex and that complexity matters. A two dimensional airflow over a simple airfoil is not the same thing as a three dimensional flow over a surface of revolution. You've introduced to the conversation, data which refers to the latter. You appear not to understand the very material you are trying to use to support your argument.
I'm not sure what you mean about Cd values "meaning it is valid for other uses, not just aircraft fuselages". Can you explain what you mean?
As for the bits I've highlighted in bold. I suggest you try and restrain your condescension until you've made quite sure that you're the one who knows what's going on.