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Routinely exceeding limitations is not a good business practice with planes. It will bite you in the arse eventually, or worse the guy who flies it last. Your attitude towards what you think the limits of the aircraft should be based on what one guy did with a brand new airplane would not for a long combat career make.
Airspeed installation error, out diving the enemy (Zeros in your one example - does not mean they dove to their max speed every time) is not as convincing to me as it is to you. From knowing what I do about Zeros I would not be anxious to get one fast in a shooting match as I would feel like I was running around with my skirt up asking to get spanked. Terrible roll rate and very stiff stick is not it's forte, so when a P40 rolled over and took the elevator down I would let it go (which would further reinforce the speed in dive advantage) but doesn't mean the Allied pilot was doing 500+.
Cheers,
Biff
I've read a couple times including quotes from pilots that flew them that getting into the uper 300s in an A6m was asking for trouble including posible structural damage.Hello Schweik,
You got me on the bad math thing. 1000+500+500 = 2000 pounds, not 1500 pounds!
Your lightened P-40L would be just past the 10,000 pound maximum T-O weight (for the late P-40) with a 2,000 pound bomb load but under the right field conditions, it sounds plausible.
The diving issue and trim that I was describing wasn't a matter of just reducing control force. It was a being aware that the aircraft may go sideways very quickly and break up. There needs to be some rudder control remaining to counteract the yaw tendency BEFORE the aircraft goes sideways.
I actually had not missed Grayman's post regarding procedures and dive speed limitations.
Please observe that what is listed in the table is max permissible dive speeds and they are not at full throttle.
Manifold pressure is not stated, but engine speed is only 2600 RPM.
Just for comparison's sake, note that the A6M3 has a maximum diving speed of 410 MPH and the A6M5 has a 460 MPH maximum and these were some of the lightweights that the P-40 fought.
- Ivan.
True but that would be a constant for all aircraft so any comparisons should still be valid, no?I think some forgets that the ASI is not that accurate at high speeds, like in a dive.
I think some forgets that the ASI is not that accurate at high speeds, like in a dive.
I've read a couple times including quotes from pilots that flew them that getting into the uper 300s in an A6m was asking for trouble including posible structural damage.
Not saying your wrong but but when you listed 460 mph as a max dive speed for them it certainly perked my interest. Could you elaborate?
I guess it had a much higher maximum dive speed than earlier modles?A6M5 is the later war model with the shorter wing
True but that would be a constant for all aircraft so any comparisons should still be valid, no?
True, any manufacturing shortcomings in airspeed indicators would varry by manufacturer but the physics that caused what seems to be universal inaccuracy at higher speeds would be.... well universal right?I know of installation error, but would not assume it's linear from one plane to the next (different types). Or the same type if airspeed indicators were made by different manufacturers.
Cheers,
Biff
I guess it had a much higher maximum dive speed than earlier modles?
I think it means risk of blackout due to G forces at the very least.
The dive characteristics of the P-40 are no mystery. There was no compressibility or flutter, no real problems with the control. It was the same issue on takeoff at full power - you had to use a lot of rudder and you needed to trim it out to be comfortable.
I've read a couple times including quotes from pilots that flew them that getting into the uper 300s in an A6m was asking for trouble including posible structural damage.
Not saying your wrong but but when you listed 460 mph as a max dive speed for them it certainly perked my interest. Could you elaborate?
True, any manufacturing shortcomings in airspeed indicators would varry by manufacturer but the physics that caused what seems to be universal inaccuracy at higher speeds would be.... well universal right?
That the p40 did or did not have a particularly inaccurate airspeed indicator and that this could be used to discount high speed readings to a greater degree than other aircraft would seem to be a seperate issue.
And quite an interesting one i would love to know about. I've never heard or read about the Warhawk having a particularly faulty airspeed indicator but that certainly does not mean that this was not the case.
I think a desirable quality in a fighter is that its main controls actually control the aircraft in a dive above 450 mph.
If you're diving at 460 mph ASI - barely controlling your aircraft with trim and I'm behind you at 500 mph ASI with light and effective ailerons/elevator and moderately heavy rudder ... sounds like a sticky situation for you.
Yes ive read that quote about the speed of the Helcat and Corsair. Always wondered if it were indeed true.Hello Michael Rauls,
There is a really nice story by Corwin Meyer about the speed difference between the Corsair and Hellcat (or lack thereof).
His claim is that it was due to the different locations of the static pressure port on the two aircraft. Airspeed is determined by the difference in pressure between the port at the end of the pitot which is facing into the direction of the airflow and the static port.
The problem he ran into was that under certain flight conditions such as low forward speed and a yaw which presented the static port into the air flow, the ASI would read near Zero.
The point is that if the airflow is not what is expected, the readings may not be what is expected.
it is pretty hard to find a nice clean location to put the sensors that does not get some odd airflow at some speeds.
My understanding is that this is the reason that there are often corrections in the aircraft manual for the readings of the ASI.
When these old and not so sleek propeller planes were going fast, often the local airflow would hit transonic speeds even if the entire aircraft was no where close to the speed of sound. These effects of "compressibility" were somewhat hard to predict and would often put shock waves or reverse airflow past odd parts of the airframe and result in nose tuck, loss of lift, loss of control effectiveness, reduction in stability, etc. Depending on location they may also be giving some odd readings to sensors that are supposed to read outside air pressure.
- Ivan.
Any chance we could make this a poll?
Only took 4 months, but there you go...