- #1
eaglestrike
- 21
- 0
Hello everyone
This is my first post. I am currently making a simulation of a P-51 Mustang in Blender3d. ("www.blender.org"[/URL]) as the other ones are from the Wright section of the NASA website as well.
If someone could explain these in simple terms for me (as I am only a tenth Grader) (or just tell me how to get the Static pressure, as that's the main problem) it would be appreciated.
The Lift and Drag calculations are from [PLAIN]http://wright.nasa.gov/airplane/lifteq.html" [Broken].
This is my first post. I am currently making a simulation of a P-51 Mustang in Blender3d. ("www.blender.org"[/URL]) as the other ones are from the Wright section of the NASA website as well.
If someone could explain these in simple terms for me (as I am only a tenth Grader) (or just tell me how to get the Static pressure, as that's the main problem) it would be appreciated.
The Lift and Drag calculations are from [PLAIN]http://wright.nasa.gov/airplane/lifteq.html" [Broken].
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