X-48B BWB Prototype to Fly in 2006, page 3
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reply posted on 29-11-2005 @ 12:46 PM by Figher Master FIN
Originally posted by Murcielago


The picture the Intelgurl posted is a good one, because it shows (by color) where the passengers will sit. So no, they dont sit in the wings.
I'm not sure about what their dimensions will be...if it ever goes commercial.
I believe any airport that can handle a 747, will also be able to handle the BWB.

heres it super imposed over the 747.


C-Thru


Most of the renderings and wind tunnel tests i've seen have 3 engines on the back...but some have had 2 or 4 engines, and a few rare(r) ones actually have the engines under the little stubby wings...which I'm sure wont be where they would be placed.



Yes, these is a piece of art, and shows the skill of engineering... But to make planes with a size like this is totally useless... The samller planes have great advantages agint these huge giants... They are more mobile, wich means that you can land on samller airfields, and not just on large ones (like with the giants) isn't the point with travelling to get from point A--->B as fast as you can, not as cool as you can...


reply posted on 15-12-2005 @ 06:32 PM by orionsgaze
i found this website rather interesting... however paranoid it may seem.

www.aircrash.org...

"Improved survivability has existed in a design called the Lifting Body for over 70 years. That design was conceived and first reduced to practice by Vincent Justus Burnelli in the early 1921 with the RB-1. Nine other Burnelli planes were built over the years through 1945.
The documentation shows that a conspiracy (note: this is not a theory) has prevented the Burnelli Company from building its superior and safer lifting body aircraft since 1941. This web-site will show you a great (and growing) number of documents proving our allegations."


reply posted on 2-9-2006 @ 10:08 AM by ch1466
Pretty Airplane but I see some problems looming.

1. While you can probably 'wing back' some structural gains by not having to loadpath especially the outboard panels for underwing engine installation, you are also going to gain weight in two other areas: CG penalty on the aft fuselage engine weight and landing gear footprint.

2. All that skin, while it may cover a neat bit of internal volume, will not come for free in terms of added airframe costs. Also, having it well forward on a thick inner fuselage/body section which /also/ functions (presumably) as a lifting body is going to spoil the cruise point Mach numbers. Indeed, you may well find that the differences in RNumber across the various sectional and root to tip factored airfoil profiles makes you have to design the airframe for different cruise points, possibly spoiling cruise drag altogether. Possibly increasing the amount of difficulty faced in controllability in other regimes. Changes in an/dihedral and sectional twist or washout may further spoil the cruise regime.

3. There is a reason for having long nose:tail separations and big verticals in that it gives the cockpit volume a reason to be as a function of doin' that magic pilot-bleep. IMO, while an advanced FBW could likely control the airframe in 80% of normal flight conditions, airliners must fly more often than other airframes in the 100% of expected weather and particularly landing conditions. I am generally sceptical of putting engines aft of a thick forebody, even on a shortchord 'fuselage' basis and can think of a lot of conditions wherein backflips and wallow leading to a runaway yaw-off as a functoin of aerodynamics could lead to the need to use power on to regain directional control in a regime where you _really_ don't want to be monkeying with the throttles due to exotic airflow considerations (assuming you can get a FADEC to react fast enough on a monster fan like that).

4. Finally, I would have to see aft body flows and structural underpinings for the tanker mission (those auto-booms/hose reels may have to go a long ways out) before I signed off on that '1 of multi' justification (I also suspect the viability of spanwise vice north/south tank bladder loadings as a function of total cargo vs. offload volumes).
And I would further like to see how they plan-to-deplane large cargo volumes in the secondary deployment-transport mission. The unfamiliar configuration and size of the airframe may make ground stance and particularly height off-ground deceptive for loading while the need to accomodate primary structural frames as well as deep cross struts/frame bulkheads for the stiff tail booms and the landing gear wells may inhibit a ventral/rear door configuration. Dedicated C-jets may be darn near worthless aerodynamically but the one thing they give you over CRAF for instance is the ability to roro from both ends of the tube without heavyweight AGE in the form of pallet lifts or bulk conveyors.


KPl.

[edit on 2-9-2006 by ch1466]
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