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I assume you mean during the war and earlier right? Because from what I remember the F-8 had a very good rate of roll...Navy airplanes have never been sparking rollers ... by design intent.
I thought the requirements called for good roll-control at low-speed with low stick movement?The old "Flying Characteristoics of Piloted Naval Aircraft" Mil-Spec tells it like it is. VERY specific requirement for roll, pitch, and ywa, none of which wille ver set world records ... but all of which contribute to fewer carrier accidents.
There's a difference between peak roll rate and initial roll response. A plane with full tiptanks might achieve a high sustained roll rate, and yet have a sluggish initial response due to the inertia of accelerating all that distributed mass in a rotational direction. It's the sluggish initial response that's fatal if you get upset on short final to the carrier.I was thinking about something: The F9F's fuel-tanks actually increased roll-rate because it affected vortex formation
TrueThere's a difference between peak roll rate and initial roll response.
That makes sense, but the F9F's tip-tanks were not able to be jettisoned, which makes me wonder why.A plane with full tiptanks might achieve a high sustained roll rate, and yet have a sluggish initial response due to the inertia of accelerating all that distributed mass in a rotational direction. It's the sluggish initial response that's fatal if you get upset on short final to the carrier.
But inadequate at low-speeds...The FW 190 is famous for being a good roller, but it is within a specific speed range ... admittedly decently wide.
I'd love to see itSomeone in here MUST have a copy they can reach and read.
You mean low response to control stick movement? I always thought they had to be quite responsive...Perhaps it was "Flying Characteristics of Manned Naval Aircraft." It has been years since I read it, and I waws shocked at how low the required responses were.
If I recall the F6F had a decent roll-rate, though not spectacular, with an excellent turn and climb-rate...It went a LONG way to explaining why the Hellcat flew the way it flew
It had a torque-stall at first and bad spin traits right?and why the Corsair was initially rejected for carrier service.
You don't want jettisonable tiptanks on a carrier aircraft. What happens if one goes and the other doesn't? Stuff like that happens. Manageable on a 250 ft X 10,000 ft runway, not so much on a pitching carrier deck crowded with explosive-laden aircraft. Besides, that ever-thirsty turbine just about guarantees you'll almost never land with any fuel left in the tips.True
That makes sense, but the F9F's tip-tanks were not able to be jettisoned, which makes me wonder why.
My question is would it be suitable for carrier use without it? This isn't the F9F-6 but the straight wingers
THE NAVY IS ALWAYS RIGHT!The Navy always DID have thin skin, and still does.They'd rather fight than admit being wrong, ayntime, ever.
Do you know why?The Navy always DID have thin skin
I could imagineDoesn't make them less effective, but it makes it hard to deal with the Navy.
Do you know why?
I feel qualified to speculate, having been there and seen it from the inside.Have NO idea why.
Will not speculate, but criticism is not something the Navy tolerates well. Well, that was 1980s.
Maybe different today? Can't say.