I do that on 0.049" and thicker wall tubing. Thinner stuff I mostly use tin snips.I meant I don't know anyone that uses a hole saw on steel tube.
I do that on 0.049" and thicker wall tubing. Thinner stuff I mostly use tin snips.I meant I don't know anyone that uses a hole saw on steel tube.
1/32 front to back? Can you see a 32nd?that applies to gas welding, you want a slight gap because of the massive heat.TIG is completely the opposite. Very small concentration of heat and the filler is much more precise.
“Giving a darn” has nothing to do with creating a gap for heat expansion. You can still create a beautiful saddle joint and actually give a darn while simultaneously making a slightly lose fit.
A loose fit has nothing to do with perfection. A loose fit is created with intention, not giving a darn is a character trait, usual a undesirable trait anywhere around a airplane.
You should always want to do the best you can because it spills in to other areas of building. Again, if you read what was written it’s still a matter of a about 2 minutes on a joint which isn’t exactly demanding on a person. My joints are tight on TIG and slightly loose on Gas Welded fuselages. All my fuselages have been accurate anywhere you measure them to probably within a 1/32” of Inch front to back. Not because of trying hard but because I give a darn. It takes no more energy to care about quality.
"Perfection is the enemy of the good" Napoleon1/32 front to back? Can you see a 32nd?
Really? LOL
Have been guilty of that in the past, but Have since got over that, I blame it on the cabinet maker in me lol"Perfection is the enemy of the good" Napoleon
I believe you would calculate the tear-out/bearing of the bolt of the hole of each tube, the tension failure of the x-section of area of the metal each tube, the (single or double) shear of the bolt.. The least value of the three calculations is the tension value.......depending on the span/length of the tube in compression this value may or may not be higher or lower than the compression calculation (Euler calculation) of the tube. Professional stress consultation for a more detailed answer, limit load test or test to destruction for real peace of mind.How about if the tube is in tension overall between the two end holes?
Sure it wasn't Joe Stalin?"Perfection is the enemy of the good" Napoleon
For me, checking data is a disease - as here:Sure it wasn't Joe Stalin?
That’s good enough for me.Voltaire quoted an Italian proverb in his Dictionnaire philosophique in 1770: "Il meglio è l'inimico del bene"
Napoleon's dates were 15 August 1769 – 5 May 1821
No, but many attribute to Stalin a quote expressing a related sentiment:Sure it wasn't Joe Stalin?
Pure geniusThat’s good enough for me.
BJC
After 11/9/89, it doesn't matter. Sorry, Uncle Joe; you lose."Noted. Does an F-4 have more capability than ten MiG-23s?"
There is a quote from a Nazi General that goes something "a Tiger tank is worth 10 Sherman's, unfortunately the Americans always have 11".No, but many attribute to Stalin a quote expressing a related sentiment:
"Quantity has a quality all its own."
This attribution is disputed. But during the Cold War it certainly seemed, to many, to be a key chracteristic of Soviet military materiel procurement.
"The F-4 is a better plane than the MiG-23."
"Noted. Does an F-4 have more capability than ten MiG-23s?"
Ironically the Sherman was a better tank, but mythology dies hardThere is a quote from a Nazi General that goes something "a Tiger tank is worth 10 Sherman's, unfortunately the Americans always have 11".
I've never heard anyone say that. It was almost a match for very early Panzers, not the Tiger. Smaller gun with less velocity, much less armor, and slower to boot. In your estimation, what made the Sherman better, aside from numbers?Ironically the Sherman was a better tank, but mythology dies hard