A aviation & planes forum. AviationBanter

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.

Go Back   Home » AviationBanter forum » rec.aviation newsgroups » Military Aviation
Site Map Home Register Authors List Search Today's Posts Mark Forums Read Web Partners

More long-range Spitfires and daylight Bomber Command raids, with added nationalistic abuse (was: #1 Jet of World War II)



 
 
Thread Tools Display Modes
  #151  
Old September 18th 03, 07:42 PM
Guy Alcala
external usenet poster
 
Posts: n/a
Default

Peter Stickney wrote:

I'm back, but an ahem, "flying visit" Trade Show season for us is
coming up, and I've just shaken off a 48 hour attack of the 24 Hour
Ebola...

In article ,
Guy Alcala writes:
The Revolution Will Not Be Televised wrote:


snip

I've managed to latch onto a few Spitfire Pilot's Notes.
Specifically, the Mk V/Seafire II/III, the Mk XII, the Mk XIV, and the
Seafire Fr. 46. (No Mk IX yet, dangit!) I'll gove more exact quotes
tomorrow, but I'll sum up a bit here, as appropriate.


snip Spit XIV tank sequence comments

Two at a time, not in squadron/wing formations, and not having to take off in IFR
conditions and climb above clouds on instruments. It was recommended to send them
to Malta singly, but Park preferred two so that if one had problems, the other
would have some idea where the a/c went down, so they might have some chance of
rescuing the pilot.


Oddly enough, the Spit V notes has an appendix to th handling
instruction for the 29 gallon fuselage tank/170 gallon super drop tank
combination. A few salient points: The aircraft is restricted to
straight and level flight until the drop tank and the rear fuselage
tank are empty. There are a lot of warning about how setting the fuel
cocks wrong will case teh system to siphon fuel overboard. The
sequence of use was to take off on the main tanks, switch to the
drop tank and run it dry (indicated by the engine cutting out - the
Spitfure Fuel gages must have been designed by the same bloke who did
the MG oil gage. Lucas, I think his name was.) The the rear tank is
emptied, (Same fuel gage), then the mains. The drop tank may be
jettisoned at any time, as long as you're straight and level, empty,
full, or in between. Nothing but straght and level until the rear
fuselage tank empties.

So - while it appears that the 29 gallon tank wa only intended to be
used with the 170 gallon tank for the Malta reinforcements, there's
really no reason why it might not have been considered, with the
proviso that you couldn't fly a real formation, or engage in combat
until it was empty, or that it couldn't be used with one of the
smaller "combat" tanks. Note though, that the 90 imp. gallon tank is
also restricted to straight and level flight.

That's a bit more flexible than I thought it would be.


I don't understand your conclusion. The pilot's notes essentially say it can't be used
for combat, which is exactly the _inflexibility_ I've been talking about. Did I get lost
somewhere? BTW, that fuel usage sequence sounds like a pure ferry setup for max. range,
unless the fuel feeds are vastly different between the Mk. V and later a/c. You'd want
to empty the drop first and retain the internal fuel, so that you could drop the external
tank for minimum drag if the winds were worse than predicted. Otherwise, for handling
purposes you'd want to empty the aft tank first, as with the Spit XIV notes.

snip much Gavin/Guy back and forth

On that basis, the use of the 29 gallon rear fuselage tank can't be
ruled out on the basis that the RAF preferred not to use it. If we
left it to RAF institutional preference alone there wouldn't have been
any rear fuselage tanks at all, but then nor would there have been PR
Spitfires to start with.


I think the Mk. IX could probably have gotten away with a 29 gallon tank or
something in that range, even with the original tail. I have serious doubts that
the Mk. V could have. Tuttle's comments imply negative longitudinal stability with
ANY fuel in the tank, and that means it is of no help to us for increasing fighter
combat radius. We could put the same fuel in a larger drop tank (at somewhat
higher drag, to be sure), say 120 gallons; the handling will be better than with
the rear tank, and it's a much simpler solution.


See above. I was rather surprised myself. The 90 gallon tank is
pretty much out as anything but a ferry tank,


I'm not sure what you mean by this. It seems to have been carried for combat missions
fairly routinely by Spits VIII/IX/XVI (indeed, the handling trials of the Spit XIV say
the a/c has no range without one, although that a/c admittedly has a more forward Cg than
the Merlin Spits), and while you certainly wouldn't want to get in combat with the thing
attached, it doesn't seem to have made the a/c longitudinally unstable by itself
(neutral, maybe), when full. It was certainly less Cg shift than carrying 66 or 75
gallons aft of the pilot's armor plate.


but an intermediate
choice of a 50 or 60 gallon tank would provide the same fuel capacity
over the 30 gallon combat tank as the aft fuselage tank would, without
much in the way of bad effects. (Didn't the Hurricane use a 50 gallon
teardrop or torpedo shaped tank? It might even be less draggy than
the 30 gallon blister.


Guy

  #152  
Old September 21st 03, 05:12 AM
Peter Stickney
external usenet poster
 
Posts: n/a
Default


Drifting through the correspondence file, which had been placed at the
bottom of the Tiger's cage.

In article ,
(The Revolution Will Not Be Televised) writes:
On 2 Sep 2003 21:09:04 -0700,
(Guy alcala) wrote:

The only effort to do this that I can see came with the
"super-Stirling" using Centaurus engines mooted by Shorts in 1941.
The Centaurus wasn't going to appear in adequate numbers in time to
have an impact on Stirling usage in the real world, meanwhile in
1941-42 the MAP and AM were unhappy with Short's chronic failure to
meet existing Sitrling production targets. Any new type or equipment
change which would further hinder production seems to have been
dismissed out of hand, although that's conjecture on my part in the
absence of hard evidence.


Green says they were supposed to get new wings of 135 ft.(!) span.


And the Wellington was upgraded to become the Warwick.... Have you
seen the thickness of the Stirling's existing wing? Even moving the
tips out for greater wing area is going to leave it struggling with
poor engine output at altitude and serious airframe weight issues.
No, what you really wanted was improved engines and extended wings,
with the emphasis on the former. Yes, that's right, Sabre-engined
Stirlings blackening the sky with their trails of carbonised oil and
ingested engine components [delusional ranting edited by men in white
coats]


A couple of points - the Warwick has always struck me as one of those
"It's nice, but why?" airplanes. It really didn't do anything that
other airplanes did better. By the time it came off the line, the
RAF's Medium bombers were teh B-25 and B-26, (Excuse me, Mitchell and
Marauder) except in those parts of teh world where the Wellington was
still viable. The Oceam Patrol stull has being handled by the
Catalina, the Sunderland, the Liberator, the Fortress, and the
U.S. Navy's patrol forces. So why all the effort? Was it an
Industrial Policy Effort to keep Vicker's Geodesic Structures skill
up to par, in case there was an urgent need to rebuild the R-100?

As for the Stirlig's wing thickness. It's not all that bad, really.
It's just, lke the B-24 and the Davis Wing, that they stuck it onto
that godawful fuselage. (Which ended up being mainly empty space,
anyway.) It's not like Critical Mach Number improvement is going to be
high on the list of Stirling Improvements. As for teh altitude
perfomance of the Hercules, in the VI and XVI models, they really
weren't all that different than the corresponding Merlin XX-24 series,
epsecially in terms of cruise power.

Sabre engined Stirling? If you're not careful, MI-? shall be visiting
you, sir, to see why you'd wish to damage the War Effort so.

--
Pete Stickney
A strong conviction that something must be done is the parent of many
bad measures. -- Daniel Webster
  #153  
Old September 21st 03, 06:04 AM
Peter Stickney
external usenet poster
 
Posts: n/a
Default

In article ,
(The Revolution Will Not Be Televised) writes:
On Wed, 17 Sep 2003 01:38:38 -0400,
(Peter
Stickney) wrote:

I'm back, but an ahem, "flying visit" Trade Show season for us is
coming up, and I've just shaken off a 48 hour attack of the 24 Hour
Ebola...


The excuses an engineer will come up with in order to lock himself
into a darkened room with his slide rule....


Well, we all have our faults.

I've managed to latch onto a few Spitfire Pilot's Notes.
Specifically, the Mk V/Seafire II/III, the Mk XII, the Mk XIV, and the
Seafire Fr. 46. (No Mk IX yet, dangit!) I'll gove more exact quotes
tomorrow, but I'll sum up a bit here, as appropriate.


Peter, I've scanned the whole Mk IX Pilot's Notes for you and Guy, but
my last attempt to send you extracts bounced due to lack of space on
your mail account. I can't put them up on a website at the moment, so
I can only email them. Contact me at -



if you have another account I could send the scans to you at.


I do, and I shall.


[rear tank in Mk XIV]

So, it was there, and it was a somewhat useful amount of fuel, but it
really wasn't considered a good thing.


The FR XIV was the only XIV to get rear tanks, the fighter version
with rear tanks mutated into the Mk XVIII when it started to be
produced on the XIV production lines in the summer of 1945.

There's no doubt that that this represents further evidence of
institutional RAF intolerance to longitudinal instability caused by
rear fuselage tanks to my mind, and it reflects the post-war position
as indicated by Pilot's Notes instructions for other versions of Spit
with the rear tanks.

I can certainly accept that this institutional intolerance existed, as
I have been asserting that from the start of my contributions to this
thread, but as I've said to ACdre Alcala, that intolerance needs to be
balanced against operational need: the the case of the Spit IX/XVI
and Mustang IV, the RAF accepted rear fuselage tankage at the price of
instability for pressing operational reasons. As soon as the war ends
and those operational reasons no longer apply, the institutional norm
will obviously reassert itself. Where I think we should be careful is
using post-war, peacetime evidence of this dynamic and reading it back
into operational service requirements where evidence exists that the
RAF was prepared to compromise their attitude.

I'd love to see the Pilot's Notes for the Mustang IV, as I suspect
they will have some interesting comments on handling and use of the
rear-fuselage tank.


Would you settle for the RAF Mustang III Pilot's Notes? I managed to
land a copy of those, as well. WRT the fuselage tank, the procedures
and warnings are teh same as those for the USAAF: Burn teh fuselage
tanks down below 40 gallons before switching to the drops, and avoid
fighter-type maneuvers befire then. It's interesting to note the
difference in the wording, between the two aircraft. The Spit is
definitely in the "Don't do anything!" category, and the Mustang is in
the "We really don't recommend this, but..." form. No admittedly, the
Mustang's fuel tank position is much better, in terms of its effect on
stability, and the Mustang was a bit more stable than the Spit to
begin with. I wonder how much of this is the manufacturer's bias
leaking through.


[snip Spit V with 170 gal overload tank and 29 gal rear fuselage tank]

Nothing but straght and level until the rear
fuselage tank empties.


Yes, but this is for an aircraft in ferry trim, and I don't think any
larger conclusions can be safely drawn when it's CoG standard was so
different from ordinary aircraft (no cannon, radios repositioned, etc)


True, but ferry trim in thas case includes the 1225#
Mondo-Pregnant-Guppy ferry tank, which had its own bad effects.
Adding the Hispano guns actually moves teh CG forward - those long
barrels & springs & things add weight forward, so that will make
things better. The Browning Guns have most of their weight in the
breech, and move teh CG aft. So, A Spit Vc with 2 Hispanos could
still work.

So - while it appears that the 29 gallon tank wa only intended to be
used with the 170 gallon tank for the Malta reinforcements, there's
really no reason why it might not have been considered, with the
proviso that you couldn't fly a real formation, or engage in combat
until it was empty, or that it couldn't be used with one of the
smaller "combat" tanks. Note though, that the 90 imp. gallon tank is
also restricted to straight and level flight.

That's a bit more flexible than I thought it would be.


My thinking was for an extra 29 gallons for early formation flight on
the climb for maybe 20 minutes, with any remainder contributing to the
flight reserve fuel load. As Guy has pointed out, rear fuselage
tankage capacity which comes at the expense of stability cannot be
considered optimal or even tolerable for combat conditions. In
response my contention is that the requirement is for endurance
coverage of long oversea flights out over the North Sea to potential
combat areas over Holland and Germany in the summer of 1943, and the
29 gallon tank in addition to the 90 gallon drop tank would increase
the operational radius in this respect, even if the combat endurance
when the aircraft got there was minimal.


Actuall, the 29 gallons would basically get you through your 20
minutes form-up and climb. Merlins tend to be a bit thirsty at that
point, burning something on the order of 80-100 Imp. Gal/Hr.

The 90 gallon tank is pretty much useless as a combat tank. Again, no
maneuvering flight allowed, and teh tank's to be punched off
immediately when emptied. Not much use if you're in Bad Guy Country.

A 29 gallon fuselage tank, combined with a less-disruptive and more
tactically useful 50 or 60 gallon tank will give about the same amount
of fuel as the 90 gallon tank, without (after the fuselage tank's been
used) the combat restrictions, and the extra drag of teh 90 gallon
tank.

But was it? After all, with no armament, the Cg moved forward. No radio (mounted
aft of where the cameras would be) moves it forward again. And quite early, they
got external fuel, in 30 gal. blister tanks under the wings.


Not only that, but a PR Spit wasn't expected to be maneuvering - It's
job was to be as high as possiblem where nobody had any maneuver
margin. They'd get to height as soon as possible after tankeoff, and
stay there.


On the other hand they were required to evade contact with
manoevreability when required. PR pilots were always expected to drop
external tanks on contact.


Yabbut, evading contact with maneuverability in this context consists
of seeing the Me (Fw's aren't going to get that high) coming up, and
making a course correction such that the interceptor has to make a
major change to cut you off. The changing again. Where there wasn't
much of a speed advantage, they can't get up to height in time to
catch you, amd, with an Me 109, you can very well run him out of gas.
If ye does goet up high, dogfighting isn't the high-G high-powered
affair that it is in the thicker air below 20,000'. Instantaneous G isn't
very high - on the order of 1.5-2 G, at best, and speed bleedoff is
pretty high. It's more of an Elephant Ballet than cut-and-thrust
fencing.


A good chunk of the aft fuel would get burned off in the
climb. It's also worth noting that the PR Spits had no disposable
load other than fuel. On the fighter Spits, the ammunition was aft of
the CG, (but not too much) and contributed to any stability problems.


There's also the issue of aft ballast, which varied greatly over the
life of the Spitfire, and over the lifespan of individual marks. The
V is a case in point, and where the equipment loading becomes
bewildering.


Yep. The thing with teh ballast, though, is that since its fixed, its
effects are predictable. It's teh shifting of weight around that's
the problem.

See above. I was rather surprised myself. The 90 gallon tank is
pretty much out as anything but a ferry tank,


Ah, but it was actually used by Spitfires and Seafires (with even
worse CoG issues than the Spit V) in combat operations. Examples
include Salerno and Normandy. There was a slipper-tank version and a
later torpedo-tank version. I suspect they would have been used
despite the tank shortcomings: the stability problems would lessen as
the fuel was consumed, and the 8th AF fighters demonstrated that
unpressurised, unreliable paper-mache tanks still could give a useful
benefit to escort radius.


Still a big drag hit, though.

the USAAF 108 gallon tanks weren't, strictly speaking, paper-mache,
they were "fiber impregnated with resin", or, in more modern terms,
epoxy over a cardboard form.

but an intermediate
choice of a 50 or 60 gallon tank would provide the same fuel capacity
over the 30 gallon combat tank as the aft fuselage tank would, without
much in the way of bad effects. (Didn't the Hurricane use a 50 gallon
teardrop or torpedo shaped tank? It might even be less draggy than
the 30 gallon blister.


They actually used a 45 gallon slipper tank as well as the 30 and 90
gallon versions. The 44 gallon Hurricane tank was an unpressurised,
unjettisonable ferry tank, with one carried beneath each wing to give
88 gallons ferry capacity. I have actually seen a photo of a Spitfire
on Malta with an improvised 2 x 44 gallon fuselage tank, although I
suspect this was a local modification made possible due to the
presence of old Hurricane ferry tanks from ferry flights from
Cyrenaica and the lack of the newer slipper tanks until later in 1942.

Whatever happened, the tanks were going to be jettisoned before
initiating combat, so I don't think the 90 gallon tanks - which should
be substantially emptied and consequently lighter before the aircraft
got to the prospective combat area anyway - would in those
circumstances impose as much of a performance restriction as we might
suppose.


True - I was thinking in terms of a way to add 90 gallons to a Mk V's
fuel capacity (Which would be about 50% of total fuel anyway) withoug
the stability and drag penalties that the 90 gallon tanks imposed.
(It's not much good being an escort fighter if you cruise slower than
the bombers that you're escorting.) To my ming, 29-30 gallons
internal, with another 60 or so external would about do it, especially
if the 60 gallon tank has no restrictions.


Remember, I'm not asserting that any of this was an optimal solution
for long-range escorting, or could have competed with aircraft that
were better suited to expanding their internal fuel capacity. I'm
trying to work along the lines that would be dictated by operational
neccessity and addressed with existing equipment and experience in
certain circumstances.


Well, in htat case, gin up a 60 gallon tank, and add teh 2 13-gallon
leadig edge tanks. The 80 gallon tank would give you about 40% of teh
total fuel, allowing it to be empty before the target area is reached,
and the 13 gallon tanks can be swapped in as a Deport-level job. They
fit in the leading edge outboard of the 20mm gun bays. but inboard of
the .303s, and slotted in between a pair of ribs. That sort of
sheet-metal work would be well within what they could do withoug a
need fr a factory-level rebuild.

--
Pete Stickney
A strong conviction that something must be done is the parent of many
bad measures. -- Daniel Webster
  #155  
Old September 21st 03, 06:48 PM
Alan Minyard
external usenet poster
 
Posts: n/a
Default

On Tue, 16 Sep 2003 23:07:09 GMT, Guy Alcala
wrote:

Alan Minyard wrote:

On Mon, 15 Sep 2003 05:35:43 GMT, Guy Alcala

Ah, well, one more for the killfile. Trolls, loons and (as in this case)
just plain rude and crude all get in.

Guy

And your language in this post would qualify as what?

Al Minyard


Let's see, not rude and crude (I suppose my posting it publicly rather than
privately could be considered rude), nor is it a troll, and I presume you
aren't implying that I'm a loon. What did you think it was?

Guy

I would think that rude would cover it. I was feeling a bit
contentious when I wrote that.

Al Minyard
  #156  
Old September 22nd 03, 02:17 PM
Peter Stickney
external usenet poster
 
Posts: n/a
Default

In article ,
(ArtKramr) writes:
Subject: More long-range Spitfires and daylight Bomber Command raids,
with added nationalistic abuse (was:
From:
(Peter Stickney)
Date: 9/20/03 9:12 PM Pacific


A couple of points - the Warwick has always struck me as one of those
"It's nice, but why?" airplanes. It really didn't do anything that
other airplanes did better. By the time it came off the line, the
RAF's Medium bombers were teh B-25 and B-26, (Excuse me,


Peter as you well know in those days we flew whatever would fly. I never heard
of a crew refusing to fly a plane because they didn't like the wing thickness.
Every mission we flew was a maximum effort. Everything that could fly did fly.
That's why.


Art, at the aircrew level, you're absolutely correct. You fly the
airplanes that your unit is issued, and you do your damnedest to be
effective. And yes, that's the way that it has to be.

There's other considerations, though, at higher levels of command.
Just as you as an aircrewman have an obligation to use the weapons you
have as effectively as possible, to accomplish the tasks of your slice
of the war, the people at the higher echelons have the obligation to
see that you have the most effective weapons practicable, and are
assigned the targets that make the best use of the capabilities of
your airplanes and crews toward winning the war. At the mid levels,
say, in the World War II case, the Eighth or Nonth Air Force levels,
that means making sure that you have the proper aircraft, (For
instance, concentrating the on the B-26 for the ETO medium bomber
force, rather than the B-25) and making sure that those aircraft are
supplied with fuel, parts, weapons and ammunition needed to get the
job done, and that the support crews, from the Air Base Civil Engineer
to the guy that's scrubbing the garbage cans, is providing a system
that means that when a mission is on, all the tasked airplanes and
crews are ready to go. (That also means making sure, as much as
possible, that losses in both aircrew and airplanes are sustainable -
that you're not losing more people and airplanes than you can replace.

That was one of the failings of the Lusftwaffe. They could, and did,
produce replacement machines for their losses. Basically, in the ETO,
the entire Luftaffe fighter force was destroyed and replaced 3 times
in 1944. They could replace the machines, but they couldn't, for
reasons as varying as the policy of not rotating the Experten home to
pass on their knowledge to the new pilots, to the gutting of the
flight training system to be wasted trying to fly supply flights to
Stalingrad and Tunisia, to the policies about training in general,
menat that the Luftwaffe's fighter arm had a thin shell of
irreplacable veterans surrounding a soft core of low-time unskilled,
and vulnerable New Guys. Each time the Luftwaffe, after husbanding
its resources, and launching another futile "hammer blow" that was to
knock the RAF and USAAF out of the war, they lost most of the new
recruits, and a fair number of the old guys. By 1945, they had
airplanes parked all over Germany - on airfields, in forests, under
bridges, at repair depots, everywhere. But not anywhere enough pilots
to fly them. By that time, they didn't bother repairing damaged
airplanes. If the pilot came back, they just issued him a new one.
That's unsustainable.

So, where I,m going with this ramble, is that, moving back to the
highest levels, where the production decisions are made, there's a
responsibility to be spending the reseources available (Time,
production capacity, raw materials, money) so that the best possible
weapons are available to accomplish the missions that you're
assigned. For example, somebody I got to know, a bit, was
Gen. Harrison Thyng (Now passed on). He was a very interesting man,
with quite a distinguished career, an Ace in both WW 2 and Korea.

In WW 2, he was a member of the 36th Fighter Group, one of the first
American units to deploy to England. The American fighters available
at that time, the P-39 and P-40, weren't considered viable in the
cross-channel war going on at that time, and they couldn't escort
B-17s into France, let alone Germany. The 36th FG was equipped with
Spitfire Mk Vs, and ended up being sent to North Africa as part of
Operation Torch. He later flew P-47s in the Pacific. That experience
gave him a certain persoective on how Industrial Policy affects Combat
Effectiveness.

During the Korean War, he was Commander of the 4th Fighter Interceptor
Wing, at that time the sole F-86 unit in Korea, flying the only
airplane that could meed the Soviet/Chinese/DPRK MiG-15s on an even
basis. (75 Sabres vs. 750 or so MiGs) They had everytning hard
charging fighter pilots needed - A good airplane, skilled, agressive,
experienced pilots, and a lot of targets, They only lacked one thing -
- There was a horrendous shortage of spare parts. The 4th FIW was, at
that time, only able to keep about half their airplanes Mission
Capable.
Despite requests through the Usual Channels, the priority for Sabre
spares was to Continental U.S. bases units. It's not that spares
weren't available, they weren't being sent to where the fighting was.
It took a personal message from Thyng to the Chief of Staff of the Air
Force that the spares situation was such that "The maintainance of Air
Superiority over Korea was in doubt" to shake people loose and get the
support that the Far East Air Force needed to flow into that
direction. Needless to say, that gave him a bit of persoective on the
responsibilities of the command echelons to provide the support needed
to see that the tools were available to carry out the assognments they
gave.

In the situation I mentioned of the VIckers Warwick, It's a question
of, in this case, the British government allocating resources
efficiently. The Warwick was intended to be the replacement for the
Wellington medium bomber. By the earliest time it could possibly be
ready, RAF Bomber Command had determined that twin-engined medium
bombers weren't suitable for the night bombing campaign. The tactical
air forces, who were conducting the medium bombing campaign, knew
that airplanes with the performance of the Wellington adn Warwick
weren't going to be sustainable in the day bombing that they were
using. They used Lend-Lease B-25s and B-26s to accomplish their
missions. For some reaon, the Air Ministry continued Warwick
production, and they scrambled around looking for someplace to use it.
The Warsicks eventually ended up being use as Air-Sea Rescue aircraft,
carrying droppable lifeboats. While this was a laudable task, it
could also have been (and, in fact was) filled by using the same
flying boat types that the RAF Coastal Command used, and by fitting
war-wary heavies, such as Lancasters, with lifeboats. Is it worse
planning to not build airplanes you know will be useful, or to build
airplanes that you know will be useless?

--
Pete Stickney
A strong conviction that something must be done is the parent of many
bad measures. -- Daniel Webster
  #158  
Old September 23rd 03, 06:45 PM
The Revolution Will Not Be Televised
external usenet poster
 
Posts: n/a
Default

On Sun, 21 Sep 2003 00:12:09 -0400, (Peter
Stickney) wrote:

A couple of points - the Warwick has always struck me as one of those
"It's nice, but why?" airplanes.


Good point. The Lancaster and Halifax were in production and had been
operationally proven by the time the Warwick started to appear. I
presume it clung on due to some production commonality with the
Wellington plant which allowed Vickers at Brooklands to cling on to
stubbornly turning out at least a few of their own design before the
MAP could bear down on them and get them to change over to Lancasters.

It really didn't do anything that
other airplanes did better.


Or even as well.

By the time it came off the line, the
RAF's Medium bombers were teh B-25 and B-26, (Excuse me, Mitchell and
Marauder) except in those parts of teh world where the Wellington was
still viable. The Oceam Patrol stull has being handled by the
Catalina, the Sunderland, the Liberator, the Fortress, and the
U.S. Navy's patrol forces. So why all the effort? Was it an
Industrial Policy Effort to keep Vicker's Geodesic Structures skill
up to par, in case there was an urgent need to rebuild the R-100?


Probably due to all the expense and effort of getting the original
machine tools on line to produce the Wimpey airframes. Writing off
that stock would have been painful after all the problems they had in
1937-39 actually reaching Wimpey production targets.

As for the Stirlig's wing thickness. It's not all that bad, really.
It's just, lke the B-24 and the Davis Wing, that they stuck it onto
that godawful fuselage. (Which ended up being mainly empty space,
anyway.)


It's waaay thicker than the Lib wing - the wing root is practically as
deep as the fuselage. I suspect, knowing wartime working practices at
Shorts, that t was used as a bunk for snoozing workmen during
construction.

It's not like Critical Mach Number improvement is going to be
high on the list of Stirling Improvements. As for teh altitude
perfomance of the Hercules, in the VI and XVI models, they really
weren't all that different than the corresponding Merlin XX-24 series,
epsecially in terms of cruise power.


The Stirling III and Halifax III still seem to have a major
differential in terms of operational ceiling, which I can only put
down to structure weight and the wing.

Sabre engined Stirling? If you're not careful, MI-? shall be visiting
you, sir, to see why you'd wish to damage the War Effort so.


True, given the total failure of Napier to even reach production
targets, let alone type reliability tests, we'd have no engines for
them anyway given that we already have several dozen Typhoon airframes
being churned out to sit in purgatory storage while Napier get their
act together. We could always use the airframes as the world's
heaviest glider or something equally critical to winning the war.

Gavin Bailey

--

Another user rings. "I need more space" he says.
"Well, why not move to Texas?", I ask. - The ******* Operator From Hell

  #159  
Old September 24th 03, 10:16 AM
Guy Alcala
external usenet poster
 
Posts: n/a
Default

The Revolution Will Not Be Televised wrote:

On Sun, 21 Sep 2003 00:12:09 -0400, (Peter
Stickney) wrote:

A couple of points - the Warwick has always struck me as one of those
"It's nice, but why?" airplanes.


Good point. The Lancaster and Halifax were in production and had been
operationally proven by the time the Warwick started to appear. I
presume it clung on due to some production commonality with the
Wellington plant which allowed Vickers at Brooklands to cling on to
stubbornly turning out at least a few of their own design before the
MAP could bear down on them and get them to change over to Lancasters.

It really didn't do anything that
other airplanes did better.


Or even as well.

By the time it came off the line, the
RAF's Medium bombers were teh B-25 and B-26, (Excuse me, Mitchell and
Marauder) except in those parts of teh world where the Wellington was
still viable. The Oceam Patrol stull has being handled by the
Catalina, the Sunderland, the Liberator, the Fortress, and the
U.S. Navy's patrol forces. So why all the effort? Was it an
Industrial Policy Effort to keep Vicker's Geodesic Structures skill
up to par, in case there was an urgent need to rebuild the R-100?


Probably due to all the expense and effort of getting the original
machine tools on line to produce the Wimpey airframes. Writing off
that stock would have been painful after all the problems they had in
1937-39 actually reaching Wimpey production targets.

As for the Stirlig's wing thickness. It's not all that bad, really.
It's just, lke the B-24 and the Davis Wing, that they stuck it onto
that godawful fuselage. (Which ended up being mainly empty space,
anyway.)


It's waaay thicker than the Lib wing - the wing root is practically as
deep as the fuselage. I suspect, knowing wartime working practices at
Shorts, that t was used as a bunk for snoozing workmen during
construction.

It's not like Critical Mach Number improvement is going to be
high on the list of Stirling Improvements. As for teh altitude
perfomance of the Hercules, in the VI and XVI models, they really
weren't all that different than the corresponding Merlin XX-24 series,
epsecially in terms of cruise power.


The Stirling III and Halifax III still seem to have a major
differential in terms of operational ceiling, which I can only put
down to structure weight and the wing.


snip

A better operational ceiling comparison would be between the Stirling III
and Halifax II, as the latter has the original 98(?) foot wing (some
sources claim that early Halifax IIIs had the original wing; I don't have
enough info to say). The Halifax II is still better but not much, and I
expect the difference is largely due to the lower weight, and maybe the
drag of the Stirling's nose turret.

Guy


  #160  
Old September 24th 03, 11:26 AM
The Revolution Will Not Be Televised
external usenet poster
 
Posts: n/a
Default

On Wed, 24 Sep 2003 09:16:49 GMT, Guy Alcala
wrote:

The Stirling III and Halifax III still seem to have a major
differential in terms of operational ceiling, which I can only put
down to structure weight and the wing.


snip

A better operational ceiling comparison would be between the Stirling III
and Halifax II, as the latter has the original 98(?) foot wing (some
sources claim that early Halifax IIIs had the original wing; I don't have
enough info to say). The Halifax II is still better but not much, and I
expect the difference is largely due to the lower weight, and maybe the
drag of the Stirling's nose turret.


[quick driveby]

The early Halifax II's (i.e. those produced throughout 1941-42) had
the Mk I nose turret, and clocked in at 34,980 lbs with an auw of
60,000lbs with a 98 ft 8in wingspan. The Stirling III seemed to come
in at something like 42,000lbs with auw's somewhere over 60,000lbs
(figures I have vary between 61,000 and up to 70,000lbs), so there's a
couple of tons of weight difference before the operational load gets
included.

The Stirling Mk III couldn't get above 17,000 feet (a couple of
thousand feet below routine operational heights for the Halifax), and
had a lower rate of climb than the Halifax. Early Halifax Mk IIIs did
have the shorter-span wings before they got the extended 103 ft 8in
wingspan.

Gavin Bailey

--

Another user rings. "I need more space" he says.
"Well, why not move to Texas?", I ask. - The ******* Operator From Hell

 




Thread Tools
Display Modes

Posting Rules
You may not post new threads
You may not post replies
You may not post attachments
You may not edit your posts

vB code is On
Smilies are On
[IMG] code is On
HTML code is Off
Forum Jump

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 09:14 AM


All times are GMT +1. The time now is 05:38 AM.


Powered by vBulletin® Version 3.6.4
Copyright ©2000 - 2025, Jelsoft Enterprises Ltd.
Copyright ©2004-2025 AviationBanter.
The comments are property of their posters.