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#1
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The 12 has a composite Glass - Balsa - Glass Fuselage
that is probably at least 0.75 inches thick. It is a very, very sturdy structure. The 12 would probably be airworthy with either the glass alone or the wood alone. Laminated together, it is a tank. |
#2
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Mark Grubb wrote:
The 12 has a composite Glass - Balsa - Glass Fuselage that is probably at least 0.75 inches thick. It is a very, very sturdy structure. The 12 would probably be airworthy with either the glass alone or the wood alone. Laminated together, it is a tank. The designer of the ASW 12 also designed the ASW 24, for which he was awarded an OSTIV prize for his contribution to safety. I'm tempted to believe he learned a lot between the 12 and the 24. Some features, like the very stiff cockpit rails, glass, Kevlar, and carbon construction, and a "soft" nose, are not present in the 12. It would be interesting to hear his opinion (and those of other knowledgeable people) on the relative merits of the two fuselage constructions. -- Change "netto" to "net" to email me directly Eric Greenwell Washington State USA |
#3
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I have had a couple of very heavy landings/groundloops in my LAK 12
('12). Comments after the first one, which involved a tree and resulted in lots of paperwork, is that no German glider would have survived with no damage. Thank goodness for Eastern Block over-engineering. Clinton Birch LAK 12 |
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#5
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I think you were misled by the "12" in the subject line, because the '12
Mark and I were referring to is the ASW 12. It's quite unlike the LAK 12, which is basically an ASW 17. As far as "over-engineering" goes, I've looked at the LAK 12, and I didn't see anything special about the design of the cockpit, which seemed to share all the design features and problems of gliders designed in the 70's. The cockpit design is the part of the glider that interests this pilot the most when it comes to crashing. I did understand you were referring to the ASW 12. Beautiful glider but I have never had the chance to see one. I used the string to refer to the LAK 12 because it is also incredibly strong - I should have added a :-) when I referred to the LAK 12 as a '12. I apologise if my understanding of the term "over-engineering" is different from that associated with the term elsewhere in the world. I used it to express the common disbelief in the engineers' calculations. It is the exact opposite of "beautifully-engineered" which would be used to express amazement at the fine calculations used to manufacture a piece with no excess or waste (Lennie would appreciate "beautiful-engineering" but despise "over-engineering" :-) ). The use of extra material just in case the engineers' calcs are incorrect is "over-engineer" e.g. using a piece 2" thick when the engineer says 1" is more than adequate. The LAK appears to have been constructed with that principle in mind and the result is an incredible tough aeroplane - like most things built by the old Eastern Block countries. You should see the suspension system on the LAK T4 trailers - could have come off a T62 tank! The LAK 12 manual does say the glider has a crashworthy cockpit but I agree that there isn't the beautiful design found in modern AS gliders with their strengthened cockpit structures. I think it is considered crashworthy because it is so thick. It is a common mistake to say the LAK 12 is basically an ASW 17. The two have similar profiles and wingspans but the wing profile is closer to the Nimbus 2 (Wortman FX67) than ASW 17 (modified Wortmann FX62). The details are actually more Jantar 1 than anything German. The LAK 12 has a single piece wing, which is very different from the Nimbus 2 or ASW 17, which have 2 piece wings. What is similar is the docile handling and performance - although at higher speeds the ASW 17 should run away from the LAK. The LAK 12 was designed at a time that the ASW 17 and Nimbus 2 were already being replaced by the ASW 22 and Nimbus 3 respectively. It was designed as a training glider for the Russians (future airforce pilots and government sponsored clubs), rather than a competition machine. Off the topic - the weather bureau are predicting 4m/s thermals and 17 000ft cloud base. A bit of a poor day as earlier in the week they were saying 6m/s and 20 000ft. Looks like the old LAK will have to stretch its legs tomorrow. Eat-your-heart-out all those in the Northern Hemisphere! Clinton Birch LAK 12 |
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#7
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Clint,
You are confused. I have visited the LAK factory. As a result of this visit I can't agree with you views on 'over engineering' of LAKs. The LAK 17/19 is under engineered. The spars appear flimsy and the cockpit has no real protection at all. In fact, one of them broke up at low level during a test flight and just about killed the pilot. If I had to crash a glider I would want to be sitting in an ASW27 or 28. The Germans calculate, design and test in order to get things right. Over engineering is fine if you are building tanks, not gliders. Mike X01 At 07:42 04 November 2004, wrote: I have had a couple of very heavy landings/groundloops in my LAK 12 ('12). Comments after the first one, which involved a tree and resulted in lots of paperwork, is that no German glider would have survived with no damage. Thank goodness for Eastern Block over-engineering. Clinton Birch LAK 12 |
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As I sadly recall, over-engineering means adding unnecessary
complexity; adding unnecessary material is over-building. Ian At 11:36 05 November 2004, Mike Hessington wrote: Clint, You are confused. I have visited the LAK factory. As a result of this visit I can't agree with you views on 'over engineering' of LAKs. The LAK 17/19 is under engineered. The spars appear flimsy and the cockpit has no real protection at all. In fact, one of them broke up at low level during a test flight and just about killed the pilot. If I had to crash a glider I would want to be sitting in an ASW27 or 28. The Germans calculate, design and test in order to get things right. Over engineering is fine if you are building tanks, not gliders. Mike X01 At 07:42 04 November 2004, wrote: I have had a couple of very heavy landings/groundloops in my LAK 12 ('12). Comments after the first one, which involved a tree and resulted in lots of paperwork, is that no German glider would have survived with no damage. Thank goodness for Eastern Block over-engineering. Clinton Birch LAK 12 |
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Mike Hessington wrote:
You are confused. I have visited the LAK factory. As a result of this visit I can't agree with you views on 'over engineering' of LAKs. No, he's not confused. You are. The LAK-12 is an over-engineered tank. I've seen a LAK-12 make it through a botched takeoff with a few scratches, that would have reduced many other gliders to a pile of debris. With all that over-engineering, the one-piece wing of the LAK-12 weighs only a few pounds more than the inner panel of the similar ASW-17 wing. The LAK 17/19 is under engineered. The spars appear flimsy and the cockpit has no real protection at all. In fact, one of them broke up at low level during a test flight and just about killed the pilot. The LAK-17/19 are entirely new designs that have nothing much to do with the 12. The the spar looks flimsy because it is made of pultruded carbon rods. It is as strong or stronger than wings made using traditional composite spar techniques. The 17/19 cockpit area has several layers of Kevlar. It is not a "safety" cockpit like the newer Schleicher and DG designs, but it is certainly safer than many older German designs. I believe the LAK-16 that crashed had a traditional spar... If I had to crash a glider I would want to be sitting in an ASW27 or 28. I agree, I wish I could afford one. The Germans calculate, design and test in order to get things right. Over engineering is fine if you are building tanks, not gliders. The LAK-17/19 have several innovative design/safety features that the Germans haven't managed to pick up on with all of their fine engineering. I have some real issues with the factory about their post-sale support, but I think the basic structural design of the LAK-17A we own is as good as the DG-303, Ventus B, ASW-20B, and Duo Discus (which was among those needing spar repair, BTW) I've also owned. I've flown my LAK-17A in some of the strongest conditions in the world, and it hasn't broken up on me yet... Marc |
#10
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Does anyone have more information on the "low level breakup" of a LAK-17/19
referred to in the Mike Hessington post? Ray Warshaw 1LK At 11:36 05 November 2004, Mike Hessington wrote: Clint, You are confused. I have visited the LAK factory. As a result of this visit I can't agree with you views on 'over engineering' of LAKs. The LAK 17/19 is under engineered. The spars appear flimsy and the cockpit has no real protection at all. In fact, one of them broke up at low level during a test flight and just about killed the pilot. |
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