- This topic has 0 replies, 1 voice, and was last updated 12 years, 11 months ago by
Douglas Krohn.
Viewing 1 post (of 1 total)
Viewing 1 post (of 1 total)
- The forum ‘Archives 2013’ is closed to new topics and replies.
Forums › Archives › Archives 2013 › Fin Design
Is there any consensus of most efficient fin geometry design in the Mach 1-2 region at the higher altitudes. I want to build a sustainer that would fly in that range starting at about 15-20k ft. Not worried as much about fin flutter at uber high speeds. Any suggestions?
Thx
Doug Krohn
L3