Comments by "Solo Renegade" (@SoloRenegade) on "Ed Nash's Military Matters"
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@ChucksSEADnDEAD "They don't deteriorate in the desert. They deteriorate by being flown" clearly you don't know what a "hangar queen" is. People in aviation do.
The A-10s are not at end of life. they've been rebuilt and upgraded and are basically new again, many decades of service left in them.
"If you're going to rebuild the entire thing, you're buying a new aircraft." and that's what they did, replaced all the old worn out items, brand new wings, new engines, new avionics. All the fatigued parts were replaced. clock has been reset.
" A total waste of money because everyone knew this would happen." but the money has already been spent, so why scrap them?
"Aircraft are built to be lightweight so they flex and strain with flight hours, depressurization and landing/take off cycles. Your Cessna's never exceed speed is what, 170 knots? Make it pull 7-8 Gs at 280 knots like an A-10 and see what happens." I'm a mechanical engineer. You're wrong. an airplane designed to withstand higher Gs has that factored into the design, to withstand that fatigue and stress accordingly. If the A-10 was designed to handle 7Gs, pulling 7Gs wont degrade its useful life. Pulling less will extend its life though. The Cessna was designed to withstand ~+3G/-1.5G, and so long as you stay within that, you're fine. But that's why they replaced the wings, not just on the a-10, but the f-15s as well. Exceeding limits can result in damage or premature failure later on. But when expecting to take higher loads, you design accordingly. You can even make high stress components with near infinite fatigue life if you us the right materials in critical places and size them correctly.
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@Aqua Fyre Convergent Evolution is the term we use in engineering. Multiple engineers designing for the same set of goals, given a certain state of technologies, materials, understanding of aerodynamics, etc available at the time, tend to result in similar solutions to the same problem. Hundreds, even thousands, of airplanes were designed around the world in the 1930s and 1940s. It is inevitable that some would share similar solutions. But the Zero was revolutionary when it was designed and first made operational, and no one can prove, with actual evidence, that the design was in any way copied from any other specific aircraft other than superficially.
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@sergeychmelev5270 SBD, A-36A, Ju-87, Typhoon/Tempest, P-47, P-39, P-40, Hurricane, F4U, Mosquito, FW190, P-38, A-1, etc.
IL-2 top speed was 250mph, service ceiling was 16k ft, rate of climb was 1000fpm, lacked maneuverability, was vulnerable from below (Hartmann's favorite way of shooting them down).
Many post-WW2 civilian airplanes perform better than this, and on far less HP too.
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