![]() |
| If this is your first visit, be sure to check out the FAQ by clicking the link above. You may have to register before you can post: click the register link above to proceed. To start viewing messages, select the forum that you want to visit from the selection below. |
|
|||||||
|
|
|
Thread Tools | Display Modes |
|
|
|
#1
|
|||
|
|||
|
On Thu, 21 Aug 2003 00:27:07 +1000, "Geoffrey Sinclair"
wrote: [snip yet more tiresome rationality and logical discourse] I will drop this in since I have not seen it elsewhere, From the British history Design and Development of Weapons, M M Postan, D Hay, J D Scott. [snipadoodledo] B was the airframe developed from the abortive mark III fighter, it was used for the Vc, IX and XII, and presumably XVI. The main change appears to be the "universal" wing. I doubt this makes a major difference to CoG calculations in the mark V though. Actually, I think it does for the Vb vs Vc. The longitudinal stability problems were worse in the Vb, while the Vc had some useful things to factor into consideration like re-raked undercarriage and bomb/drop-tank plumbing, not to mention a different internal wing structure which might have allowed small wing tanks. I don't think the Vb wing had that capacity due to strength issues. It seems the fighter had quite a tight margin, the report that for AB186 noting handling was worse with a Rotol propeller, rather than the standard de Havilland propeller, they were testing a modified elevator balance. Yes, but also note the constant buggering about with different ballast displacements for the different props, CSUs and fuselage equipment fitting. The Vb Trops are the worst, I think, as they carried more weight in the rear fuselage behind the existing CoG and more weight overall. BR202 (tropical Vc) was tried with a 29 gallon rear fuselage tank, requiring repositioning of the water tank, oxygen bottle and the R3002 radio, the certificate of design was issued on 7th July 1942 along with official approval. Some Spitfire Vs were flown from England to Gibraltar in early 1942, January I think, 5.5 hour flight. October 1942 was the date I have for ferry flights from Gibraltar to Malta, using the 170 gallon Boulton Paul tank and 29 gallon rear fuselage tank tested in the summer of '42. So far as I know they were all shipped to Gibraltar beforehand though, just like they were shipped to Takoradi, Egypt and later on Casablanca. The ferry Spits weren't in combat trim. Seen Morgan and Shacklady, page 150 in my copy, map of Spitfire V range with extra fuel arrangements? Yes, but this seems to be related to the October 1942 Gib-Malta ferry range, and doesn't reflect a realistic combat radius with operational load and operational fuel reserves (the escort range given would need a 5 hour endurance on external fuel and a 270 mile range on internal fuel excluding 15 mins combat allowance). I honestly have difficulties seeing any LR Spit, especially a V, getting back from Berlin on internal fuel only as that chart seems to indicate. Relying on external tankage to get into combat and return to base is a non-starter, and that's how I see that chart personally. Escort, 5 minute take off, 10 minute climb, 15 minutes maximum power, remainder cruise at 240 mph, radius 540 miles. Given the need for higher cruise and problems of slower bombers this still should have meant around the German border at least. Note the extra range required a bigger oil tank, from 7.5 or 8.5 to 14.4 gallons. Note the deeper noses on the PR versions. The book does not state what fuel tankage is being used. The extra oil was less of a problem with later single-piece engine blocks (Merlin 50 and 60 upwards). 540 miles is a problematic figure for a Mk V escort range on existing fuel, the deciding factor of which would be the range on internal fuel to get home, not just the tankage available in external stores. That's why I've been ranting about rear-fuselage tanks in the Mk V. We're still not approaching the ranges and endurance required for PR Spits, but even so the fitting of a PR XI oil tank and nose profile is entirely possible. In early 1942 Sholto-Douglas was asking for tanks of up to 30 gallons in the wings. Fighter Command had realised it needed more range to fight over France, it does not seem to have come up with the idea it should try for Germany. If BC were wedded to a daylight campaign against Germany, this would follow, pushed along by a torrent of invective in memos from Harris and the CAS. The text mentions the mark IXe weights with 66 gallon rear tank. As far as I can tell the idea of major Spitfire modifications keeps running into the problem that until the P-47 was proven the allies did not have another fighter that could be considered a match for the Fw190A and Bf109G, hence the rush for the IX instead of awaiting the mark VIII. The middle east had to do without Spitfires until early/mid 1942 (Malta then Egypt), the major withdrawal of mark IXs from fighter command to the squadrons in Tunisia in early 1943. The RAF in the MTO were still, even after Eisenhower had pushed for Mk IXs to supplement promised deliveries of Mk VIIIs in December 1942, on the short end of the stick for Mk IX allocations. What we need in this TL is a senior RAF staff constituency able to take on Fighter Command and win, in terms of dictating fighter operations, development and production. [snip basically agreed spec of LR Mk IX] [Mk VIII production figures from Postan] That gives ACM Kramer about 550 Mk VIIIs in the second half of 1943, or about 90 per month as I suspected. Gavin Bailey -- Another user rings. "I need more space" he says. "Well, why not move to Texas?", I ask. - The ******* Operator From Hell |
|
#2
|
|||
|
|||
|
|
|
#3
|
|||
|
|||
|
|
|
#5
|
|||
|
|||
|
Peter Stickney wrote:
In article , (The Revolution Will Not Be Televised) writes: On 2 Sep 2003 21:17:46 -0700, (Guy alcala) wrote: snip Vader states that the Mk VIIIs had the 'C' wing, which implies that the Mk. IXs should have been able to be given LE tanks with little difficulty. I'm under the impression that the substantive changes to the Mk. VII/VIII were in the fuselage, and except for the tanks the wings were identical. Does anyone actually KNOW what the structural/internal changes were from the Mk.V/IX etc. to the Mk. VII/VIII? We all know about the tail wheel, but there had to be more than that. I don't know, but the internal wing spars, which I suspected would show a difference, appear to be identical between the Vc and the VII, in which case there should be no problem with deleting the outboard MG positions in favour of more fuel tank capacity in the Vc-airframed IX. The shorter-span ailerons appear to be shortened at the wing-tip end. If there were any fuselage differences, they didn't stop the late-production IXs getting rear-fuselage tanks anyway. I'm back. I've been examining cutaways & measuring & doing sums like a numerate Dervish, and, while I can't give a definitive answer, I can make the following observations: The Mk Vc wing would certainly be suitable for teh leading edge tanks. I'd go so far as to say that if you were really concerned about volume in that area, ditching on or both of the .303 guns in each wing would open up a bunch of space, withoug compromising much in the way of firepower. I don't think that's necessary, as the exploded view of a Mk. XIV in Price's "Spitfi A Documentary History" shows the L.E. tanks are inboard of the cannon. If tanks could also be installed outboard in place of the MGs, then I'd probably go for it and accept the somewhat greater vulnerability in combat, but just getting standard Mk.VIII tankage (123 Imp. Gal. total) would be fine for a start. The big deal with the Mk V, and volume behind the cockpit, is that hteat's where the radios live. Going with a smaller/lighter set would allow something like teh Mk IX's 29 Imperial Gallon tank. Not sure what you mean here, as the Mk. VCs were given a 29 Imp. Gal. ferry tank for the Gib-Malta ferry flights. The later Mk. IX/XVI had 66 Imp. gal. rear tanks. Note that on the Mk IX, the only way to keep the CG acceptable with the aft tank was to use it only in conjunction with one of the belly tanks. H'mm, at least with the Mk. XIV, the Cg moves aft when drop tanks are carried, not forward. See http://www.fourthfightergroup.com/ea...41weights.html I don't really view that as a big deal for an escort fighter, unless you expect to be engaged immediately at the French Coast. The recommended tank sequence would be, after takeoff, to use the aft fuselage tank, then the external tank. (I keep wanting to call that marsupial-looking excrescence the "carbuncle", for some reason) The 29 Imp Gal tank should last somewhere between 15 minutes to 1/2 hour, depending on power settings, so that gets you through form-up, climbout, and pretty much across the Channel. Part of the pilot's notes for the F./F.R. XIV are online, and the FR. XIV flight restrictions contains the following statement: "On F.R. Mk. XIV a/c it is essential, for reasons of stability, that the rear fuselage tank should be emptied before flying at altitudes in excess of 15,000 feet." It also states that the fuel tank sequence for the F.R.14 is t/o on main tanks, switch to rear fuselage tank and empty it, then feed from drop tank. See http://www.geocities.com/spades53.ge...4_notes_13.jpg ISTR that this tank is ca. 33 gallons. Guy |
|
#6
|
|||
|
|||
|
On Mon, 08 Sep 2003 05:47:33 GMT, Guy Alcala
wrote: [welcome back Peter, with your smoking slide-rule] The big deal with the Mk V, and volume behind the cockpit, is that hteat's where the radios live. Going with a smaller/lighter set would allow something like teh Mk IX's 29 Imperial Gallon tank. Not sure what you mean here, as the Mk. VCs were given a 29 Imp. Gal. ferry tank for the Gib-Malta ferry flights. The later Mk. IX/XVI had 66 Imp. gal. rear tanks. The standard fuselage Mk IX/XVI got a 75 Imperial gallon rear fuselage tank, with tear-drop canopy versions with the cut-down fuselage getting 66 gallons. My thinking was for the 29 gallon Gibraltar ferry rear tank, or something pressurised/self-sealing with a similar capacity in the LR Vc, with additional wing tankage for the LR Vc or LR VIII & IX coming from the outboard MG position's, e.g. using the E-wing armament or even 2 x Hispanos with 2 x .303 MG's in the inboard cannon position available in the C wing, while stuffing a further 10 gallons or so of fuel in the outboard MG positions, as Pete has pointed out. This would be additional to the Mk VII/VIII wing tanks with their (conservative) 25 gallon capacity which were positioned further inboard of the first cannon mounting. Total here would be for something like 35 gallons in the wings additional to the 85 gallon conventional tankage, 29 gallon rear fuselage tankage and external drop tanks of up to 90 gallons capacity. Gavin Bailey -- Another user rings. "I need more space" he says. "Well, why not move to Texas?", I ask. - The ******* Operator From Hell |
|
#7
|
|||
|
|||
|
The Revolution Will Not Be Televised wrote:
On Mon, 08 Sep 2003 05:47:33 GMT, Guy Alcala wrote: [welcome back Peter, with your smoking slide-rule] The big deal with the Mk V, and volume behind the cockpit, is that hteat's where the radios live. Going with a smaller/lighter set would allow something like teh Mk IX's 29 Imperial Gallon tank. Not sure what you mean here, as the Mk. VCs were given a 29 Imp. Gal. ferry tank for the Gib-Malta ferry flights. The later Mk. IX/XVI had 66 Imp. gal. rear tanks. The standard fuselage Mk IX/XVI got a 75 Imperial gallon rear fuselage tank, with tear-drop canopy versions with the cut-down fuselage getting 66 gallons. Right. My thinking was for the 29 gallon Gibraltar ferry rear tank, or something pressurised/self-sealing with a similar capacity in the LR Vc, with additional wing tankage for the LR Vc or LR VIII & IX coming from the outboard MG position's, e.g. using the E-wing armament Probably not an option, as we'd need the limited number of .50 cals for flexible nose guns in the Halifax IIIs, if the B-24 deal doesn't come off. or even 2 x Hispanos with 2 x .303 MG's in the inboard cannon position available in the C wing, while stuffing a further 10 gallons or so of fuel in the outboard MG positions, as Pete has pointed out. This would be additional to the Mk VII/VIII wing tanks with their (conservative) 25 gallon capacity which were positioned further inboard of the first cannon mounting. Total here would be for something like 35 gallons in the wings additional to the 85 gallon conventional tankage, 29 gallon rear fuselage tankage and external drop tanks of up to 90 gallons capacity. Seems like it would be a lot easier to boost the forward fuselage capacity of the Mk. V/IX up to 96 gallons by swapping in bigger tanks (we know there's room there), before you add all those other tanks and the associated plumbing. I agree you'd still want the L.E tanks, but let's do the easiest stuff first. The extra 11 gallons in the enlarged forward tanks buys perhaps 10 minutes of cruise coming home: let's be _real_ conservative and call it 30 miles. Then we'll also need to enlarge the oil tank at some point. The outboard tanks you describe are so small that I wonder if they're worth the weight of all the plumbing, plus the extra vulnerability (remember that these tanks feed into the main tanks after room has been made in the latter, so they won't be used in combat - no one's going to transfer fuel while they're fighting). Guy |
|
#8
|
|||
|
|||
|
|
|
#9
|
|||
|
|||
|
In article ,
Guy Alcala writes: Peter Stickney wrote: That yesterday seemed to be my day for being obfuscative. I'm back. I've been examining cutaways & measuring & doing sums like a numerate Dervish, and, while I can't give a definitive answer, I can make the following observations: The Mk Vc wing would certainly be suitable for teh leading edge tanks. I'd go so far as to say that if you were really concerned about volume in that area, ditching on or both of the .303 guns in each wing would open up a bunch of space, withoug compromising much in the way of firepower. I don't think that's necessary, as the exploded view of a Mk. XIV in Price's "Spitfi A Documentary History" shows the L.E. tanks are inboard of the cannon. If tanks could also be installed outboard in place of the MGs, then I'd probably go for it and accept the somewhat greater vulnerability in combat, but just getting standard Mk.VIII tankage (123 Imp. Gal. total) would be fine for a start. The big deal with the Mk V, and volume behind the cockpit, is that hteat's where the radios live. Going with a smaller/lighter set would allow something like teh Mk IX's 29 Imperial Gallon tank. Not sure what you mean here, as the Mk. VCs were given a 29 Imp. Gal. ferry tank for the Gib-Malta ferry flights. The later Mk. IX/XVI had 66 Imp. gal. rear tanks. Ah, sorry. Don't forget that I've lagged a bit here. I was just following up on Gavin's question about squeexzing more fuel into a Mk V. Since the engine's a lot lighter, they don't have as much moment on the Good Side of the CG balance, and there isn't any good space insude a Mk V for a substantial amount of fuel. The 29 Imp. Gallon tank is all that you can get an have an airplane that isn't too dangerous for the 1943 RAF. In irder to geep that influence to a minimum, a medium-sized drop tank would also be necessary, to keep the CG where it ought to be. My point about the radios was that the early Brit TR sets were, when you include their rectifiers * transformers, about 200# of load, and quite a bit of space. If that 200# could be cut in half, that's 15 Imperial Gallons of fuel that yo could squeeze in. Note that on the Mk IX, the only way to keep the CG acceptable with the aft tank was to use it only in conjunction with one of the belly tanks. H'mm, at least with the Mk. XIV, the Cg moves aft when drop tanks are carried, not forward. See http://www.fourthfightergroup.com/ea...41weights.html Yep. Yhe Mk IX's got it nearly on the CG datum, though. I'll get the tracing paper & rulers & see if I can come up with som emore detail. don't really view that as a big deal for an escort fighter, unless you expect to be engaged immediately at the French Coast. The recommended tank sequence would be, after takeoff, to use the aft fuselage tank, then the external tank. (I keep wanting to call that marsupial-looking excrescence the "carbuncle", for some reason) The 29 Imp Gal tank should last somewhere between 15 minutes to 1/2 hour, depending on power settings, so that gets you through form-up, climbout, and pretty much across the Channel. Part of the pilot's notes for the F./F.R. XIV are online, and the FR. XIV flight restrictions contains the following statement: "On F.R. Mk. XIV a/c it is essential, for reasons of stability, that the rear fuselage tank should be emptied before flying at altitudes in excess of 15,000 feet." It also states that the fuel tank sequence for the F.R.14 is t/o on main tanks, switch to rear fuselage tank and empty it, then feed from drop tank. See http://www.geocities.com/spades53.ge...4_notes_13.jpg ISTR that this tank is ca. 33 gallons. Which is about enough to climb about 5,000' with a Griffon Spit. -- Pete Stickney A strong conviction that something must be done is the parent of many bad measures. -- Daniel Webster |
|
#10
|
|||
|
|||
|
Peter Stickney wrote:
I'm back. I've been examining cutaways & measuring & doing sums like a numerate Dervish, and, while I can't give a definitive answer, I can make the following observations: snip Spit comments BTW, I know we've been sidetracking you with work on the Spit, but were you able to run any numbers for the Lanc B.2? Guy |
|
| Thread Tools | |
| Display Modes | |
|
|
Similar Threads
|
||||
| Thread | Thread Starter | Forum | Replies | Last Post |
| Long-range Spitfires and daylight Bomber Command raids (was: #1 Jet of World War II) | The Revolution Will Not Be Televised | Military Aviation | 20 | August 27th 03 10:14 AM |