- Thread starter
-
- #141
Ad: This forum contains affiliate links to products on Amazon and eBay. More information in Terms and rules
One last note about the Arrow. There is one that survived and it is flown by Elvis but he flew into the Bermuda triangle and neither have been seen again.
I don't have the knowledge of metals and stress and fatique to talk about this on your level but maybe this link I'll provide can clear up any of the questions or doubts you or I might have as it tells what is what in retrospect to the metals. But it did complete 5000hrs of ground runningI don't know anything about this experimental engine, but suspect that the hot section lifespan was SEVERELY limited due to the metallurgy of the day. And most likely of such grave limitations as to not be of production quality. Zoom fast. Throw it away.
I don't know anything about this experimental engine, but suspect that the hot section lifespan was SEVERELY limited due to the metallurgy of the day. And most likely of such grave limitations as to not be of production quality. Zoom fast. Throw it away.
You are correct and the only thing I could say about that is the across the board hot section and TBO increase seen on military turbine engines of the period as the continued into service. I know there are dozens of J-79 TCTOs that replaced many internal parts, bearings etc that increased engine life, I would think the Iroquois would of fell into the same situation.Those of us that are passionate about the Arrow have been accused of stating how good it is without facts. Is this statement not going out of your way to say that it is a bad performer without facts?
Those of us that are passionate about the Arrow have been accused of stating how good it is without facts. Is this statement not going out of your way to say that it is a bad performer without facts?
I can't speak directly to the "hot section lifespan" as I have never heard the phrase before
Instal said:but it seems people like to assume the Arrow was no better than existing aircraft when evidence supports a different conclusion.
The first problem is obviously due to its tailess-delta configuration. Without canards it is unlikely to turn well. The second obvious problem is the lack of a wasp-waste as seen on most other Mach 2+ aircraft. This should have increased drag would have limited speed and endurance.
Diefenbaker did the best thing for the Canadian taxpayer and I do not like you folks in the US saying bad things about him for it. How would you like it if I said Lincoln's mother wore army boots, Eh?
Anyway the Avro's cockpit is exactly the same shape as my cat's head. He bites and so did the Arrow.