Brian Jackson
Platinum Member
- Joined
- Jul 17, 2004
- Messages
- 3,549
- Location
- Hamburg, New Jersey USA
- Aircraft
- GyroBee Variant - Under Construction
Hi All.
Hoping to pick the brains of some experienced builders with respect to approx. sq. ft. weights of various empennage constructions. In the preliminary design of a tail section skinned with .020" alum with generous surface areas, I'm calculating it would put the assembly well over the 20 lb. mark, with 12 lbs. just in the 020 skin alone. It's airfoil shaped with cross-bar spar tubes.
I'm entertaining the idea of using the 020 skin just from the leading edges to the spars and covering the rest with fabric. However, I don't know if this path yields any significant weight savings. Is there a "rule of thumb" for sq. ft. weight of cloth & dope coverings? And any practical knowledge from those who have experience in this area?
Originally a composite tail seemed attractive but I don't see how it would be lighter than aluminum. Any guidance would be appreciated. Thank you.
Respectfully,
Brian Jackson
Hoping to pick the brains of some experienced builders with respect to approx. sq. ft. weights of various empennage constructions. In the preliminary design of a tail section skinned with .020" alum with generous surface areas, I'm calculating it would put the assembly well over the 20 lb. mark, with 12 lbs. just in the 020 skin alone. It's airfoil shaped with cross-bar spar tubes.
I'm entertaining the idea of using the 020 skin just from the leading edges to the spars and covering the rest with fabric. However, I don't know if this path yields any significant weight savings. Is there a "rule of thumb" for sq. ft. weight of cloth & dope coverings? And any practical knowledge from those who have experience in this area?
Originally a composite tail seemed attractive but I don't see how it would be lighter than aluminum. Any guidance would be appreciated. Thank you.
Respectfully,
Brian Jackson