This article is within the scope of WikiProject Physics, a collaborative effort to improve the coverage of Physics on Wikipedia. If you would like to participate, please visit the project page, where you can join the discussion and see a list of open tasks.PhysicsWikipedia:WikiProject PhysicsTemplate:WikiProject Physicsphysics articles
This article is within the scope of the Aviation WikiProject. If you would like to participate, please visit the project page, where you can join the project and see lists of open tasks and task forces. To use this banner, please see the full instructions.AviationWikipedia:WikiProject AviationTemplate:WikiProject Aviationaviation articles
This article has not yet been checked against the criteria for B-class status:
Referencing and citation: not checked
Coverage and accuracy: not checked
Structure: not checked
Grammar and style: not checked
Supporting materials: not checked
To fill out this checklist, please add the following code to the template call:
Latest comment: 9 years ago1 comment1 person in discussion
Does the zero lift axis depend on airspeed? I think the article should answer this question. — Preceding unsigned comment added by 24.244.32.56 (talk) 05:48, 22 January 2015
In any incompressible flow around an airfoil there is no reason to expect the orientation of the zero-lift axis to vary with different flow speeds. In transonic, sonic and supersonic flows around an airfoil the orientation of the zero-lift axis is likely to vary with Mach number. I haven't looked for a published source for my views. Dolphin(t)06:14, 22 January 2015 (UTC)Reply