There is information here on different wing construction types:
wing | main spar | construction note | 1940 | 0363 | Flight Archive
"The principal advantage of the single-spar wing is
that it is an easy production job. The spar and nosing
can be built as separate units, and need not remain long
in an assembly jig. The rear portion of the wing can be
attached afterwards, and, as the strength of this is not
so important, detachable panels can be included to facilitate
erection. Present examples of this type of construction are the
Spitfire, Hampden, Flamingo, and Heinkel 112."
There are secondary spars but they carry little of the load or are there to attach constrol surfaces to. One advantage of the Spitfires single spar wing may have been that under load it twisted in such a way as to increase washout and thus reduce stall. The FW 190's much stiffer two spar wing twisted less, but in the wrong direction. Roll is important: if it takes you a second or two longer to do a role into a split s or to bank into a turn having a smaller turn radious may be a mute point: your enemy will be fully into the turn and one step ahead.
The Mk. 20 wing structure was designed to be much stiffer and this was to improve roll rate, extra armament options may also have been a driving factor but certainly the Spitfire would have been a miserable machine with the old wing at the kind of speeds the Mk 22 was capable of.
I have found anecdotal data on Me 109 roll rate:
A Messerschmitt document (Rollwendigkeit 109 F [Me 109G]) on the
matter shows roll rate as following:
263mph 425 km/h - 84 deg./sec.
298mph 480 km/h - 95 deg./sec.
341mph 550 km/h - 109 deg./sec
Don't know if this is TAS or IAS or what altitude or what stick force without the actual report but it is better than the Me 109F2 report.
Small numbers of Me 109 were produced which had spring tabs to reduce aileron forces.
wing | main spar | construction note | 1940 | 0363 | Flight Archive
"The principal advantage of the single-spar wing is
that it is an easy production job. The spar and nosing
can be built as separate units, and need not remain long
in an assembly jig. The rear portion of the wing can be
attached afterwards, and, as the strength of this is not
so important, detachable panels can be included to facilitate
erection. Present examples of this type of construction are the
Spitfire, Hampden, Flamingo, and Heinkel 112."
There are secondary spars but they carry little of the load or are there to attach constrol surfaces to. One advantage of the Spitfires single spar wing may have been that under load it twisted in such a way as to increase washout and thus reduce stall. The FW 190's much stiffer two spar wing twisted less, but in the wrong direction. Roll is important: if it takes you a second or two longer to do a role into a split s or to bank into a turn having a smaller turn radious may be a mute point: your enemy will be fully into the turn and one step ahead.
The Mk. 20 wing structure was designed to be much stiffer and this was to improve roll rate, extra armament options may also have been a driving factor but certainly the Spitfire would have been a miserable machine with the old wing at the kind of speeds the Mk 22 was capable of.
I have found anecdotal data on Me 109 roll rate:
A Messerschmitt document (Rollwendigkeit 109 F [Me 109G]) on the
matter shows roll rate as following:
263mph 425 km/h - 84 deg./sec.
298mph 480 km/h - 95 deg./sec.
341mph 550 km/h - 109 deg./sec
Don't know if this is TAS or IAS or what altitude or what stick force without the actual report but it is better than the Me 109F2 report.
Small numbers of Me 109 were produced which had spring tabs to reduce aileron forces.