Humor Random Comments Thread

People sometimes ask, why cats are so funny, and the answer is: because if they were larger, also would be dangerous.

I used to look at our family cat, and she would look back at me, and I always figured she was thinking,

"If I were a little bigger and you were a little smaller, I'd eat you. Just sayin'.

But for now I love you as long as you feed me and give me a little ice cream now and then."
 
A bit more HOI3, not my game, but damn am I jealous.

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Speaking of LCSs...the shiny new LCS-5, USS Milwaukee, had an "engineering casualty" and had to be towed into port for repairs 20 days after commissioning. :facepalm:

https://www.rt.com/usa/325710-littoral-ship-milwaukee-breakdown/

Some garbled information about metal filings in the lube oil system. I believe it is a CODAG system with twin screws, so I don't know what would cause a complete loss of propulsion like this, unless they had a main gearbox failure of some sort. It was either something not caught during sea trials (bad, very bad) or a flaw (bad, very bad).
 
Speaking of LCSs...the shiny new LCS-5, USS Milwaukee, had an "engineering casualty" and had to be towed into port for repairs 20 days after commissioning. :facepalm:

https://www.rt.com/usa/325710-littoral-ship-milwaukee-breakdown/

Some garbled information about metal filings in the lube oil system. I believe it is a CODAG system with twin screws, so I don't know what would cause a complete loss of propulsion like this, unless they had a main gearbox failure of some sort. It was either something not caught during sea trials (bad, very bad) or a flaw (bad, very bad).

A typical source for such problems are too small or too soft gear bolts. That kind of thing happens in the world. Usually, you have a magnetic detector at the lube oil filter to detect such problems before the gear box is completely destroyed.
 
What does CODAG mean for us not-so-cool kids?

Sorry, talking shop. :hesaid: A lot of these sorts of ships have multiple propulsion units (diesels or gas turbines) geared onto a common shaft, usually to efficiently operate between cruise speed and maximum operating speed, as well as to provide redundancy. My favorite is the COGOG system in the Russian Tarantul class missile corvette (which I actually got to see on the Hiddensee at Battleship Cove on a special engine room tour). It has two cruising gas turbines of 4000 hp, and two main gas turbines of 11,000 hp each, so you could idle around on one 4000 hp engine, or put the spurs to it and have 30,000 hp. The main gas turbines, while not really jet engines, produce enough exhaust that they deliver extra thrust, and so there are distinctive doors on the stern of the vessel that are opened when the main turbines are operated. If everything hits the fan, there is a diesel engine (same kind as used in the T-62 tank) for emergency power.
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FYI It 'gas' like in 'gas turbines', not 'gas' as the petrol in 'murican cars. :lol:

The complex gearing shown on the wiki page looks like an engineer's nightmare IMHO.
 
FYI It 'gas' like in 'gas turbines', not 'gas' as the petrol in 'murican cars. :lol:

The complex gearing shown on the wiki page looks like an engineer's nightmare IMHO.

That gearing provides a lot of operational flexibility. Normally it should reduce the probability of a casualty completely knocking out propulsion. That is what is so strange about the USS Milwaukee. Sounds like something major was shaving metal and they had to secure the shaft to prevent damage.
 
The main gas turbines, while not really jet engines, produce enough exhaust that they deliver extra thrust, and so there are distinctive doors on the stern of the vessel that are opened when the main turbines are operated.

Every turbo-shaft produces residual thrust.

In a "jet" or "low bypass turbofan", some energy is extracted from the air stream to drive the fan and compressors, but a lot of it is left, so the exhaust comes out as high velocity. Lots of thrust is produced, because F = mdot * v, with mdot being mass flow and v exhaust velocity of the engine. In addition that that, gas pressure plays a role and the gas pressure is still somewhat high.

In a turbo-shaft, the turbine drives a shaft through a speed reductor (slower RPM, higher torque). Measures are taken to extract as much energy out of the gas stream as possible. That means slowing it down, decreasing its pressure and temperature. While a lot can be done, some energy is still left in the gas stream.


In aircraft turbo-props, about 10% of the thrust is produced by the turbine, with the rest from the propeller.
 
Every turbo-shaft produces residual thrust.

Even reciprocating engines will produce some thrust with their exhaust if they are eating enough air. The Rolls Royce Merlin had rearward facing flared ejector exhausts for this reason. The Spitfire picked up about 10 knots on its top speed due to this effect.
 
Even reciprocating engines will produce some thrust with their exhaust if they are eating enough air. The Rolls Royce Merlin had rearward facing flared ejector exhausts for this reason. The Spitfire picked up about 10 knots on its top speed due to this effect.

Even cooler, the radiator housing for the Merlin on the P-51 Mustang, underneath the fuselage, was used as a sort of mini jet engine and actually produced a couple pounds of thrust instead of drag. Forgot where I read that.
 
Was there any inherent differences between the RR Merlin and the RR/Packard Merlin, or was it a 1:1 license job?
 
On Earth, curiosity drives scientists. On Soviet Mars, scientists drive Curiosity.

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Even cooler, the radiator housing for the Merlin on the P-51 Mustang, underneath the fuselage, was used as a sort of mini jet engine and actually produced a couple pounds of thrust instead of drag. Forgot where I read that.

It is pretty much exactly a ramjet, just with an alternate heat source.

If you pull up a video of a P-51 flyby on YouTube, the whistling from the P-51's little ramjet is distinctly audible.

Example: http://www.youtube.com/MCAA8BuimcE
 
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On Earth, curiosity drives scientists. On Soviet Mars, scientists drive Curiosity.

---------- Post added at 00:42 ---------- Previous post was at 00:19 ----------



It is pretty much exactly a ramjet, just with an alternate heat source.

If you pull up a video of a P-51 flyby on YouTube, the whistling from the P-51's little ramjet is distinctly audible.

Example: http://www.youtube.com/MCAA8BuimcE

That whistle is actually the gun ports in the wing acting as, well, whistles. You'll notice it's missing from "clean wing" birds like Voodoo and Strega.

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Was there any inherent differences between the RR Merlin and the RR/Packard Merlin, or was it a 1:1 license job?

Not as I recall. The Packard version was slightly reengineered to enable easier mass production.
 
That whistle is actually the gun ports in the wing acting as, well, whistles. You'll notice it's missing from "clean wing" birds like Voodoo and Strega.

It's also missing from the P-40, which also has 6 wing-mounted 50-cals. Of course, in either case, it could be missing from the videos we're looking at because of other factors, such as AOA if its the gun port or radiator settings if it's the radiator, and airspeed in either case.

The F4U had a well-known whistle that was supposed to be from the oil coolers.

I wonder if anyone has ever instrumented a P-51 with microphones placed by suspected whistle sources to try to get rock-hard data on the true whistle source. I still think radiator is most plausible, but I hear people arguing with equal vehemence for radiator, supercharger, guns, and guns + laminar flow wing.
 
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