Have the Short Stirling be more successful as a bomber aircraft for the RAF especially against the Halifax & Lancaster
Much obliged!
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Do you know how much more that would increase the aircraft's range, perhaps the RAAF could use the alt Sterling ITTL rather than the B - 24 Liberator. As perhaps the Stirling's greater ceiling could make it largely immune to most IJNAF and IJAAF fighters.For a start don't shorten the wings and artificially limit its maximum altitude. Also don't divide the fuselage Bomb bay and use the wing bomb cells as additional fuel tanks. The extended range will make the Stirling a very useful bomber in the Far East.
Yeah. To close the mid-Atlantic gap sooner.Keep the longer wings and make the changes Peg Leg Pom suggests. Put the Stirlings to use as long-range maritime patrol planes
While probably good ideas the resulting aircraft wouldn't be a Stirling but a completely different aircraft.Shorten the fuselage a lot (3-4m); Stirling have had considerably longer fuselage than Lancaster or Halifax. (saves weight)
Remove the front and dorsal turrets and respective gunners. (saves weight, lessens drag)
Have the flight crew being stationed in the nose, replace the greenhouse with the navigator's cupola. (saves weight, lessens drag)
Shorter and lighter undercarriage.
Lower weight improves service ceiling, range/radius and cruise speed, lower drag improves the improvements. The take off and landing characteristics will also improve.
As noted above, instead of the segmented bomb bay go for the unrestricted one, so the cookies can be carried.
It's reminiscent of the S.36 Super Stirling designed to meet Specification B.8/41.May I humble suggest you look at the Stirling as flown in the Peerless Air Ministry TL. This is built to the original S29 specification, long wingspan, powered by four Fairey monarch H24 engines providing 2000hp each in 1939. A very different beast to OTL. The LRMP aircraft variant had fuel in the wings instead of bomb cells and range comparable to the OTL long range Liberator!
Barnes in Shorts Aircraft since 1900 says...As noted above, instead of the segmented bomb bay go for the unrestricted one, so the cookies can be carried.
This is confirmed by the entries on Specifications B.12/36 and P.13/36 in Air Britain's The British Aircraft Specifications File.An important, and as it turned out significant, difference between the two categories was that the largest "stores" to be carried by the B.12/36 were 2,000lb armour piercing bombs, whereas the smaller P.13/36, in its tactical role, had to provide for two 21-in torpedoes. The unforeseen result of that was that the B.12/36 designs had divided bomb compartments suitable for nothing larger than 2,000-lb A.P. bombs, while the P.13/36 designs had uninterrupted bomb cells of maximum length and width.
Barnes says that the Stirling's wingspan had to be reduced from 112ft to 99ft 1in so that it could fit into existing aircraft hangars. The entry on Spec. B.12/36 says that the British Aircraft Specifications File says that the wingspan should not exceed 100ft.Keep the longer wings...
Ahhhh - the old Airfix kit. Looking at mine now, gathering dust on top of a display cabinet.
That's news to me. It could have been to save the money needed of build larger hangars rather than the cost of longer wingspans.Isn't the 'wingspan reduced to fit hangers' argument, for all the designs, discredited now and the reason is largely down to trying to keep cost down?
That's news to me. It could have been to save the money needed of build larger hangars rather than the cost of longer wingspans.
Shorten the fuselage a lot (3-4m); Stirling have had considerably longer fuselage than Lancaster or Halifax. (saves weight)
Remove the front and dorsal turrets and respective gunners. (saves weight, lessens drag)
Have the flight crew being stationed in the nose, replace the greenhouse with the navigator's cupola. (saves weight, lessens drag)
Shorter and lighter undercarriage.
Lower weight improves service ceiling, range/radius and cruise speed, lower drag improves the improvements. The take off and landing characteristics will also improve.
As noted above, instead of the segmented bomb bay go for the unrestricted one, so the cookies can be carried.
IIRC the specification limit on wingspan wasn't related to the width of the doors on the aircraft hangars but was a misguided attempt to keep the aircraft weight down. Easiest solution there is to simply specify, and enforce, the maximum weight allowed and let the designers get on with things.Have the Short Stirling be more successful as a bomber aircraft for the RAF especially against the Halifax and Lancaster.
IIRC the specification limit on wingspan wasn't related to the width of the doors on the aircraft hangars but was a misguided attempt to keep the aircraft weight down. Easiest solution there[,] is to simply specify, and enforce, the maximum weight allowed and let the designers get on with things.
And there was also the requirement that the B.12/36 and P.13/36 aircraft be capable of catapult assisted take-offs. That may have been so that they could take-off from existing grass runways and thus avoid the expense of building long concrete runways.It is worth remembering that at the time these aircraft were specified, runways were grass. Keeping size and weight down was as much about preserving this infrastructure as it was about the aircraft.
The next sentence was.Earlier in 1936, the Air Staff's technical advisers had been pessimistic about the take-off performance of heavily loaded monoplanes and had even predicted that some form of catapult launching (referred to as "frictionless take-off" device) would be essential on existing airfields; this had led to the issue of Specification B.4/36 for a bomber with assisted take-off, and Short Brothers had submitted a scheme, but expressed the view, based on their experience and expectations of the Gouge flap fitted to the Empire Boat, that such assistance was unnecessary.
In due course the flights of Canopus confirmed the earlier results obtained on Scion M-3, and Gouge had no hesitation in submitting a B.12/36 tender with a wing of 112ft span similar to the Sunderland's, which would have given an excellent high-altitude performance at the normal weight of 48,000lb and acceptable rates of climb at the "increased" and "maximum overload" weights of 53,000lb and 65,000lb respectively. Unfortunately, before ordering any prototypes, the Air Ministry stipulated that the that the span must not exceed 100ft, in order to conform to existing hangar dimensions; even this limitation was accepted by Gouge, who increased the flap chord to 48 per cent of the wing chord and hoped to obtain Hercules VI engines for production.
That's news to me. It could have been to save the money needed of build larger hangars rather than the cost of longer wingspans.
How much money would reducing the wingspan by 12% save? I think that the cost of another 13 feet of wingspan would be insignificant in relation to things like the engines and gun turrets. It's the aircraft equivalent of the "steel is cheap and air is free" theory for warships.