Quoting Pihero (Reply 50): Let's keep this discussion, civil, shall we ? |
Quoting Pihero (Reply 50): Your excel spreadsheet is so basic and so simplistic and only geared toward your demonstration, which then fails. |
Yes, let's.
Quoting Pihero (Reply 50): and of course, Boeing engineers and aerodynamicists are just a bunch of ignorant nincompoops, un able to build a,n optimum wing for the 748I ? |
Not at all my point. The 748 wing has suboptimally high sweep because it's a reloft on the bones of a '70's wing. With the 748, Boeing tried exactly what A380NEO enthusiasts recommend here: it put new engines and a stretch on a bad wing.
Quoting Pihero (Reply 50): the A380 has a wake that is not worse than a 747.
Politics and a certain measure of safety concerns still impose these separations |
This sounds like a conspiracy theory. Have any evidence that A380 has no larger wake vortices than a 747?
Here's a real-world example of exactly the type of purchase decision that you claim does not exist:
Quote: Rainey cites a higher trip cost for the A380 compared to smaller widebodies like the 787 despite comparable per seat costs as the main challenge to adding the type to United’s fleet. |
http://www.flightglobal.com/news/art...es-not-work-for-united-cfo-413079/
Quoting Pihero (Reply 50): CASM, as it is, relates to a whole airline fleet, cabin configurations for all types...etc... and only then refer to -at the said airline- cost structure and financial procedures.
CASM has never been meant for comparing airplanes ( what level of comfort, what network...etc...) |
Quoting seahawk (Reply 52): If CASM would be so important every airline would fly their planes cramped with as many Y seats as possible, the truth is they do not. |
Quoting speedbored (Reply 60): There is no point having the lowest seat-mile costs if you can't fill the seats, or don't have enough seats. |
I am grouping these responses together to address a point that some here frequently make. The commentators claim to debunk an "A.net myth" that CASM is really really really important; seems to me they propound a new myth in which basic economics doesn't apply to airlines. That's my basic response, I'll provide further details below.
As a metapoint, I'll remark that often commentators who claim to "debunk" a "myth" are granted deference for appeals to some deeper knowledge. This is a dangerous trend. No matter the level of specialized knowledge claimed by a poster, their assertions must be verified for whether they make sense. As I'll argue below, the group claim advanced in the quotes above doesn't pass this test.
Quoting speedbored (Reply 66): And then there is the problem of there not being any standard for exactly how CASM should be calculated when it is used in those comparisons. |
This is indeed a problem but it is largely surmountable. With enough time and effort, one can create a LOPA for the respective cabins based on standardized rules. One can use cabin area as a proxy, which is a good metric and even better if one adjusts for airplane-specific characteristics.
Leeham does LOPA's for all of its comparative analyses. The airwaysinsight article linked in the OP did as well. One can check the acceptability of these LOPA's against floor areas, for minimum seat width assumptions, etc.
What one should not do is claim that airplane interiors contain spaces whose dimensions and possibilities can only be reckoned in extremely specific and idiosyncratic cases, rendering moot all normal cognition of space and experience. It's not THAT difficult.
Quoting speedbored (Reply 66): I would argue that area-mile costs are probably better because it removes any suggestion of cheating on the config to favour one side or the other. |
OK! I'll mostly agree! But now we pretty much have a CASM comparison.
Quoting speedbored (Reply 66): As I said in my previous post, in my experience, airlines do not compare CASM at all when making decisions on aircraft type, because costs are only one part of the picture. |
First, see above-linked story about A380 and 787.
UA doesn't want the A380 because its unit costs (whether CASM or cost per average cabin M2/ft2) are "similar" to the 787 at much greater capacity.
Second, it simply doesn't follow that "do not compare CASM at all" because costs are "only part" of the picture. Range, cabin comfort, capacity, cargo/freight, jet/piston-engined, real/toy, plane/plain are also "only part" of the picture but are extremely important.
Quoting speedbored (Reply 66): So, for each option, they are more interested in acquisition costs, trip costs, numbers of seats in each cabin class, estimated revenues, and availability. |
-Acquisition cost is part of CASM. Unit costs that exclude acquisition are Cash Operating Costs - COC.
-Trip cost is CASM*seats
-"estimated revenues" is just RASM*seats
You haven't come close to disproving the extremely high relevance of CASM/RASM here. Each of your factors besides availability is directly related to CASM/RASM. Of course nobody disputes that the CASM of an airplane that you can't have for 6 years is irrelevant if you need that plane now.
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Does everyone know the fable/essay/meme of the hedgehog and the fox?
http://en.wikipedia.org/wiki/The_Hedgehog_and_the_Fox
The fox knows many things; the hedgehog one big thing. Each style of thought is important to ordinary life and intellectual history.
I am operating as a hedgehog here - I have one big idea: that the A380 isn't efficient enough for its size; that its inefficiency is traceable to a suboptimal wing; and that it probably could be superb if rewinged.
I'm a hedgehog in the midst of foxes, mostly. I admit to lacking specialized knowledge, I'm happy to admit when I'm wrong on a particular like wing twist. I'm appreciative of all this foxy knowledge here, even when it's presented in a context critical of me.
But so far I remain convinced that my big idea is the best of the ideas presented in this forum regarding the A380's future.
Nobody has disputed, so far, that a longer, lighter wing would dramatically improve fuel efficiency. As far as I can tell it's indisputable. The only question is - by how much?
But to have a meaningful discussion of that question, we first have to ask - what is a meaningful target of fuel efficiency delta? What level of fuel burn would create an A380NEO/NWO/PIP capable of providing ROI sufficient to justify the project?
-10%?
-15%?
-20%?
-25%?
-30%?
-35%?
-40%?
Regardless how you evaluate my aerodynamic model, the fuel burn figure, once plugged into the DOC cost, creates a CASM delta whose fundamentals are based on the best publicly available data on A380 operating costs (Leeham's).
A 17% per-pax fuel burn delta creates a ~7% CASM delta for a NEO with ~16% price premium over CEO. That's just arithmetic, not aerodynamics. Doesn't matter how you get that 17% aerodynamically or mechanically. Is that good enough to make the A380NEO sell well? I doubt it, especially if you need a stretch to get to 17%.
For those who accept the worldview that CASM/RASM and basic economics actually matter to airlines, does anyone want to venture a guess as to what level of CASM delta would materially affect A380 sales prospects?