• Welcome to the new COTI server. We've moved the Citizens to a new server. Please let us know in the COTI Website issue forum if you find any problems.
  • We, the systems administration staff, apologize for this unexpected outage of the boards. We have resolved the root cause of the problem and there should be no further disruptions.

COACC

Fritz: Yes, the B52's look suffers from the square-cube law

If you multiply the size of a device by X, you multiply it's surface area AND structural member cross-sections by x^2, but the overall mass and volume increase by x^3. Since a beam's load carrying capacity is directly proportional to it's cross sectional area (assuming no nifty design tricks or size-related flaws), you only multiply load per y units by x^2 when scaling, while the load applied usually goes up as x^3.

Of course, the SU also doesn't carry much cargo, either. The B52 does.

Off axis bracing for non-aerodynes is relevant, as well. There will always be some off axis loads when changing orientation.
 
Fritz: Yes, the B52's look suffers from the square-cube law

If you multiply the size of a device by X, you multiply it's surface area AND structural member cross-sections by x^2, but the overall mass and volume increase by x^3. Since a beam's load carrying capacity is directly proportional to it's cross sectional area (assuming no nifty design tricks or size-related flaws), you only multiply load per y units by x^2 when scaling, while the load applied usually goes up as x^3.

Of course, the SU also doesn't carry much cargo, either. The B52 does.

Off axis bracing for non-aerodynes is relevant, as well. There will always be some off axis loads when changing orientation.
 
Back
Top