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#331
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And, BTW the website is completely wrong - the rudder balances, which were at the root of the tail problems, were modified in 1943 - there was no problem with the elevator balances. From early 1944 new production Typhoons, and some earlier ones, adopted Hawker Tempest horizontal tailplanes and elevators which had a larger area - with the small tailplanes and a full weapons load of either 8 RP-3s or 1,000 lb bombs the longitudinal stability deteriorated. Your comment was the Hurricane, Typhoon and Tempest had near perfect longitudinal stability - no comment about a "longitudinal stability issue." Fact is you were wrong, once again - both aircraft were slightly unstable longitudinally. If the RAE had no standards for stability and control it meant they were unable to comment on the stability and control of aircraft they tested - read the 1938 report carefully, it is most illuminating. The Spitfire PNs describe control and g-limits in rough air and caution pilots against making high-speed manœuvres in such conditions, something also covered in Pilot's Notes General. |
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#332
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The thing that made the Spitfire instability special was the very light elevator plus the very short stick travel for large reactions, the Hawker designs were so normal in this aspect, that it isn't even mentioned.
I think for a unbiased reader it shows very clear, that in this thread everything possible is used to indirectly attack the OP. I shure hope for the same unbiased support for the other planes that hopefully will be discussed.
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#333
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I know...this is just another one of those pesky reports by that class of people who know nothing of the subjet i.e. a pilot, but at least this one doesn't have 60 years of faded memory and biassed oppinion (he also flies a 109)
http://www.vintagewings.ca/VintageNe...Rob-Erdos.aspx Quote:
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#334
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#335
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I really enjoyed reading the attached documents and opinions in this thread, thank you very much for that. Taildraggernut cheers for the Rob Erdos article, great reading.
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Bobika. |
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#336
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The problem is, that crumpp doesn't present claims, he presents documented facts!
The claims are coming from those, who are unwilling to accept those facts. To recapitulate those facts, as i understood them, in concentrated form: 1. The early Spitfire marks had a inherent longitudal instability which led to the manufacturer-fix with bob-weights. 2. The stick forces for the elevator were extraordinarily small in the Spitfire. 3. The stick travel was extrordinarily small for large reactions. It really doesn't matter how good the pilots then were able to cope with those circumstances, it should be reflected in game that the plane doesn't fly itself, but has to be flown, and that with precise, small inputs for the elevator. Also the tests shown by crumpp say that if one doesn't ride the buffet in a turn, but gets into the buffet, the turn performance is reduced drastically. It is up to the fm programmer to make it possible to feel the difference in game. Every aircraft has its quirks, and i think we want them all represented in this game.
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#337
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#338
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In turns with speeds high enough to prevent reaching maximum lift coefficient because of the excessive accelerations involved, the small static longitudinal stability of the Spitfire caused undue sensitivity of the normal acceleration to small movements of the stick. As shown by the time histories of high-speed turns (figs. 15 to 1 it was necessary for the pilot to pull back the stick and then ease it forward almost to its original position in order to enter a turn rapidly without overshooting the desired normal acceleration. Although this procedure appears to come naturally to a skillful pilot, flight records from other airplanes show, that a turn may be entered rapidly and the desired normal acceleration may be held constant by a single rearward motion of the stick, provided the static stability of an airplane is sufficiently large. By careful flying, the pilot was able to make smooth turns at high speed, as shown by figures 17 and 18. Ordinarily, however, small movements of the stick caused appreciable variations in the normal acceleration, as shown in figures 15 and 20. Quote:
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#339
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#340
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I think it is worth re-posting the words of an aeronautical engineer who spent a lifetime practicing his profession over one who hasn't:
FIGURE 4.5. Supermarine Spitfire airplane. A high-performance fighter noted for its role in the Battle of Britain and throughout WW II, the Spitfire had desirably light elevator control forces in maneuvers and near neutral longitudinal stability. Its greatest deficiency from the combat standpoint was heavy aileron forces and sluggish roll response at high speeds. http://history.nasa.gov/monograph12/ch4.htm |
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