Inverted Vantage
Formerly Unknown Target
- Joined
- Jun 19, 2008
- Messages
- 1,116
Hi everyone. I'm converting an aircraft design spreadsheet from imperial to metric measurements, and I need some help making sure it's working right.
If anyone could give me these numbers for an aircraft design that they know is correct (the units would just make my life easier, if you have them in them that would be great, just preferably at least metric);
- Lift coefficient
- Root Chord (cm)
- Tip Chord (cm)
- Length of 1/2 the wing in cm
- Stall speed
- Air density
- Lift of 1/2 the wing at stall (in kg-force)
- Lift of the total wing at stall (in kg-force and grams)
That would be AWESOME! Thank you!!!
If anyone could give me these numbers for an aircraft design that they know is correct (the units would just make my life easier, if you have them in them that would be great, just preferably at least metric);
- Lift coefficient
- Root Chord (cm)
- Tip Chord (cm)
- Length of 1/2 the wing in cm
- Stall speed
- Air density
- Lift of 1/2 the wing at stall (in kg-force)
- Lift of the total wing at stall (in kg-force and grams)
That would be AWESOME! Thank you!!!
