Re: [Flightgear-devel] [OT] BA-609, V-22 derivative aircraft

2002-12-14 Thread Martin Spott
 Martin Spott wrote:

 This does not have to be as difficult as it is with the V-22. The Osprey is
 designed for being stuffed into _very_ small space below a ship's deck.
 If they had more space then it would have been possible to improve security
 simply by increasing the wing span,
 

 The problem, I think, is not in the wing span. In transition the 
 aircraft is working around the stall speed for the wings. I would think 
 that a larger wing would decrease rather than increase stability, no?

Oh, you get heavily increased torque from the ailerons for manouverability
and you get much more lift from large wings at low speed - especially
because on the current design at least 90 % of the wing area suffers from
the down-wind generated by the two the rotors,

Martin.
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Re: [Flightgear-devel] [OT] BA-609, V-22 derivative aircraft

2002-12-14 Thread C. Hotchkiss


Martin Spott wrote:

Martin Spott wrote:



...

Oh, you get heavily increased torque from the ailerons for manouverability
and you get much more lift from large wings at low speed - especially
because on the current design at least 90 % of the wing area suffers from
the down-wind generated by the two the rotors,



Ah yes, prop wash helps improve control effectivity at low speeds. It 
isn't going to be great, but should help. So how smooth is it when lift 
become significant on the wings? The wash off the rotors should be 
strong, but very turbulent. Air flow around the wings ought to be one 
very nasty numerical analysis problem, especially near wing stall. I can 
only imagine what surprises it held for the designers.

Regards,

Charlie H.

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Re: [Flightgear-devel] [OT] BA-609, V-22 derivative aircraft

2002-12-12 Thread C. Hotchkiss


Martin Spott wrote:

The big problematic area ...  regime is unstable and
recovery difficult.



This does not have to be as difficult as it is with the V-22. The Osprey is
designed for being stuffed into _very_ small space below a ship's deck.
If they had more space then it would have been possible to improve security
simply by increasing the wing span,



The problem, I think, is not in the wing span. In transition the 
aircraft is working around the stall speed for the wings. I would think 
that a larger wing would decrease rather than increase stability, no?

Regards,

Charlie H.
--
C makes it easy to shoot yourself in the foot;
C++ makes it harder, but when you do, it blows
away your whole leg. - Bjarne Stroustrup


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Re: [Flightgear-devel] [OT] BA-609, V-22 derivative aircraft

2002-12-11 Thread Andy Ross
Carsten.Hoefer wrote:
 Forgetting about all 'unsafe' situations in helicopters, do we have
 one in flightgear? Is it possible to model one with the existing
 flight models we use?

Not without a lot of code work.  Helicopters have a bunch of effects
that don't exist in the current FDMs.

Things like asymmetric lift effects would need to be revisited. Both
YASim and JSBSim model P factor, which is what the same effect is
called on a fixed wing propeller aircraft, via a hack that isn't
general enough to handle ~90 degree AoAs.  Other stuff, like blade
flapping and precession of the main rotor just don't exist and would
need to be done from scratch.

For myself, I don't find PC simulation of helicopters very
interesting.  Existing throttles don't have anywhere near enough
precision to simulate a collective, IMHO.  Helicopter pilots maintain
altitude by feeling for very slight changes in vertical acceleration
and adjusting with tiny movements of the collective.  There's no way
we can simulate that well.  We could do it with an autopilot like
device, of course, but where's the fun in that?  You might as well
just install Commanche MCMXIV or whatnot to get same level of
simulation realism. :)

If you want to try hovering in FlightGear, try the Harrier.  That
thing is really difficult to hover, for all the same reasons that the
real aircraft is difficult to hover.

Andy

-- 
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Senior Software Engineer  Emeryville, CA
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Re: [Flightgear-devel] [OT] BA-609, V-22 derivative aircraft

2002-12-11 Thread C. Hotchkiss


Curtis L. Olson wrote:

Tony Peden writes:


--- Jim Wilson [EMAIL PROTECTED] wrote:


Hmmmthat should thin the ranks down on Wall St even more. ...   IMHO
that thing
even looks dangerous :-)


More dangerous than a helicopter?  ...

It sounds like avoiding the vortex ring state...



I think the big danger is at landing or takeoff.  ...


The big problematic area for this class of aircraft historically has 
been the transition between hover, or rotor based operation and 
flying, where the wings are important. That regime is unstable and 
recovery difficult.

Regards,

Charlie H.

--
C makes it easy to shoot yourself in the foot;
C++ makes it harder, but when you do, it blows
away your whole leg. - Bjarne Stroustrup


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Re: [Flightgear-devel] [OT] BA-609, V-22 derivative aircraft

2002-12-11 Thread Martin Spott
 I think the big danger is at landing or takeoff.  If you lose an
 engine or have any sort of mechanical failure on a single side, you
 are going to hit hard at some really odd angle.

The engines are capable to deliver _enormous_ power for a short time in case
of an engine failure - I believe this only works for a couple of minutes,
afterwards the are fried  ;-)
But their most error prone part are not the engines but the way too short
time frame for such a difficult development. Several prototypes and at least
one pre-series plane crashed because of software failures   killing
several crews and passengers  :-(((

Martin.
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Re: [Flightgear-devel] [OT] BA-609, V-22 derivative aircraft

2002-12-11 Thread Martin Spott
 The big problematic area for this class of aircraft historically has 
 been the transition between hover, or rotor based operation and 
 flying, where the wings are important. That regime is unstable and 
 recovery difficult.

This does not have to be as difficult as it is with the V-22. The Osprey is
designed for being stuffed into _very_ small space below a ship's deck.
If they had more space then it would have been possible to improve security
simply by increasing the wing span,

Martin.
-- 
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[Flightgear-devel] [OT] BA-609, V-22 derivative aircraft

2002-12-10 Thread Jon S Berndt
Bell/Agusta V-22 derivative commercial BA609:

http://www.bellagusta.com/html/aeroNet/downLoads/20393_609_AB_Brochure.pdf

Fascinating. Pretty pictures, too.

Jon

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Re: [Flightgear-devel] [OT] BA-609, V-22 derivative aircraft

2002-12-10 Thread Jim Wilson
Hmmmthat should thin the ranks down on Wall St even more.  It's hard to 
imagine they are selling civilian versions while there's talk about nixing the 
Osprey because of safety concerns.  Well maybe not that hard.  IMHO that thing
even looks dangerous :-)

Best,

Jim


Jon S Berndt [EMAIL PROTECTED] said:

 Bell/Agusta V-22 derivative commercial BA609:
 
 http://www.bellagusta.com/html/aeroNet/downLoads/20393_609_AB_Brochure.pdf
 
 Fascinating. Pretty pictures, too.
 


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Re: [Flightgear-devel] [OT] BA-609, V-22 derivative aircraft

2002-12-10 Thread Erik Hofman
Jim Wilson wrote:

Hmmmthat should thin the ranks down on Wall St even more.  It's hard to 
imagine they are selling civilian versions while there's talk about nixing the 
Osprey because of safety concerns.  Well maybe not that hard.  IMHO that thing
even looks dangerous :-)

It looks like a power ranger ...

Erik


Jon S Berndt [EMAIL PROTECTED] said:


Bell/Agusta V-22 derivative commercial BA609:

http://www.bellagusta.com/html/aeroNet/downLoads/20393_609_AB_Brochure.pdf

Fascinating. Pretty pictures, too.



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Re: [Flightgear-devel] [OT] BA-609, V-22 derivative aircraft

2002-12-10 Thread Tony Peden

--- Jim Wilson [EMAIL PROTECTED] wrote:
 Hmmmthat should thin the ranks down on Wall St even more.  It's
 hard to 
 imagine they are selling civilian versions while there's talk about
 nixing the 
 Osprey because of safety concerns.  Well maybe not that hard.  IMHO
 that thing
 even looks dangerous :-)

More dangerous than a helicopter?  That fixed wing makes me feel better
about it.  I wonder if gliding in that thing is any better than
autorotation in a helicopter ...

It sounds like avoiding the vortex ring state is doable but will
likely require a fair amount of training (and possibly some control law
mods)

 
 Best,
 
 Jim
 
 
 Jon S Berndt [EMAIL PROTECTED] said:
 
  Bell/Agusta V-22 derivative commercial BA609:
  
 

http://www.bellagusta.com/html/aeroNet/downLoads/20393_609_AB_Brochure.pdf
  
  Fascinating. Pretty pictures, too.
  
 
 
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Re: [Flightgear-devel] [OT] BA-609, V-22 derivative aircraft

2002-12-10 Thread Curtis L. Olson
Tony Peden writes:
 
 --- Jim Wilson [EMAIL PROTECTED] wrote:
  Hmmmthat should thin the ranks down on Wall St even more.  It's
  hard to 
  imagine they are selling civilian versions while there's talk about
  nixing the 
  Osprey because of safety concerns.  Well maybe not that hard.  IMHO
  that thing
  even looks dangerous :-)
 
 More dangerous than a helicopter?  That fixed wing makes me feel better
 about it.  I wonder if gliding in that thing is any better than
 autorotation in a helicopter ...
 
 It sounds like avoiding the vortex ring state is doable but will
 likely require a fair amount of training (and possibly some control law
 mods)

I think the big danger is at landing or takeoff.  If you lose an
engine or have any sort of mechanical failure on a single side, you
are going to hit hard at some really odd angle.  At least with a
helicopter you are probably going to land butt first and might have a
chance to try an autorotation.

Curt.
-- 
Curtis Olson   IVLab / HumanFIRST Program   FlightGear Project
Twin Cities[EMAIL PROTECTED]  [EMAIL PROTECTED]
Minnesota  http://www.menet.umn.edu/~curt   http://www.flightgear.org

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Re: [Flightgear-devel] [OT] BA-609, V-22 derivative aircraft

2002-12-10 Thread Jon S Berndt
On Tue, 10 Dec 2002 13:09:03 -0600
 Curtis L. Olson [EMAIL PROTECTED] wrote:


I think the big danger is at landing or takeoff.  If you lose an
engine or have any sort of mechanical failure on a single side, you
are going to hit hard at some really odd angle.  At least with a
helicopter you are probably going to land butt first and might have a
chance to try an autorotation.


I would be very surprised if the engines are not 
cross-coupled such that each engine drives both props, as 
in the V-22. A single engine failure would not cause one 
rotor to be unpowered. The gearbox for the V-22 was one of 
the main design challenges for the Osprey, IIRC. The other 
components of the drive train/propulsion system are made 
for extremely high reliability for that very reason. They 
are mostly Criticality 1 items. I agree that the big 
danger is at takeoff and landing, for sure, but it's 
because of the aero phenomena. I wonder if clever 
placement of sensors about the aircraft and some Expert 
Systems logic could potentially sense dangerous conditions 
and adapt appropriately?

Jon


Jon

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Re: [Flightgear-devel] [OT] BA-609, V-22 derivative aircraft

2002-12-10 Thread Gene Buckle
 It sounds like avoiding the vortex ring state is doable but will
 likely require a fair amount of training (and possibly some control law
 mods)


Speaking of which - a recent issue of Aviation Leak that I have mentions
that they've been unable to properly account for/simulate the VRS in the
flight simulators for the V-22.

g.



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Re: [Flightgear-devel] [OT] BA-609, V-22 derivative aircraft

2002-12-10 Thread Curtis L. Olson
Gene Buckle writes:
  I think the big danger is at landing or takeoff.  If you lose an
  engine or have any sort of mechanical failure on a single side, you
  are going to hit hard at some really odd angle.  At least with a
  helicopter you are probably going to land butt first and might have a
  chance to try an autorotation.
 
 Curt, there is a central transmission in the wing that will transfer the
 drive to the operating engine automatically so that won't happen.  If they
 both fail at once though

You could also imagine that something downstream of this central
transmission could fail, again leaving you in an unhealthy state.  I
agree with the people who are saying this can be made to fly safely
within reasonable tolerances, but I also think there are certain
phases where it's probably always going to be a little less safe than
a helicopter, or perhaps you could say that certain types of failures
at certain times would be less survivable in the BA-609 ...

Regards,

Curt.
-- 
Curtis Olson   IVLab / HumanFIRST Program   FlightGear Project
Twin Cities[EMAIL PROTECTED]  [EMAIL PROTECTED]
Minnesota  http://www.menet.umn.edu/~curt   http://www.flightgear.org

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Re: [Flightgear-devel] [OT] BA-609, V-22 derivative aircraft

2002-12-10 Thread Jon S Berndt
On Tue, 10 Dec 2002 15:22:05 -0600
 Curtis L. Olson [EMAIL PROTECTED] wrote:


a helicopter, or perhaps you could say that certain types 
of failures at certain times would be less survivable in the BA-609 

This (above) might be more true than your first statement. 
One thing that comes to my mind though, for V-22, is that 
survivability might be increased in one way due to less 
time spent in the combat area. You dash in fast, you drop 
down and pick up the downed airman, then you dash out 
fast. It's got the advantage over helicopters in that 
respect, at least. If the BA_609 proves to be as safe as 
helicopters I can see it really taking off.

Jon

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Re: [Flightgear-devel] [OT] BA-609, V-22 derivative aircraft

2002-12-10 Thread Gene Buckle
  Curt, there is a central transmission in the wing that will transfer the
  drive to the operating engine automatically so that won't happen.  If they
  both fail at once though

 You could also imagine that something downstream of this central
 transmission could fail, again leaving you in an unhealthy state.  I
 agree with the people who are saying this can be made to fly safely
 within reasonable tolerances, but I also think there are certain
 phases where it's probably always going to be a little less safe than
 a helicopter, or perhaps you could say that certain types of failures
 at certain times would be less survivable in the BA-609 ...


Well one of my favorite quotes goes something like this:

If your wings are moving faster than you are, you're in a Helicopter and
are therefore unsafe. :)

g.



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Re: [Flightgear-devel] [OT] BA-609, V-22 derivative aircraft

2002-12-10 Thread Curtis L. Olson
Gene Buckle writes:
 Well one of my favorite quotes goes something like this:
 
 If your wings are moving faster than you are, you're in a Helicopter and
 are therefore unsafe. :)

I suppose the related quote would be something along the lines of If
your wings are moving slower than you, they are probably not still
attached (and are therefore unsafe.)

Curt.
-- 
Curtis Olson   IVLab / HumanFIRST Program   FlightGear Project
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Re: [Flightgear-devel] [OT] BA-609, V-22 derivative aircraft

2002-12-10 Thread Tony Peden
On Tue, 2002-12-10 at 13:22, Curtis L. Olson wrote:
 Gene Buckle writes:
   I think the big danger is at landing or takeoff.  If you lose an
   engine or have any sort of mechanical failure on a single side, you
   are going to hit hard at some really odd angle.  At least with a
   helicopter you are probably going to land butt first and might have a
   chance to try an autorotation.
  
  Curt, there is a central transmission in the wing that will transfer the
  drive to the operating engine automatically so that won't happen.  If they
  both fail at once though
 
 You could also imagine that something downstream of this central
 transmission could fail, again leaving you in an unhealthy state.  I
 agree with the people who are saying this can be made to fly safely
 within reasonable tolerances, but I also think there are certain
 phases where it's probably always going to be a little less safe than
 a helicopter, or perhaps you could say that certain types of failures
 at certain times would be less survivable in the BA-609 ...

I don't know ... it sound like you are really starting to stack up the
failures.

 
 Regards,
 
 Curt.
-- 
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Re: [Flightgear-devel] [OT] BA-609, V-22 derivative aircraft

2002-12-10 Thread Jon S Berndt
On 10 Dec 2002 15:18:48 -0800
 Tony Peden [EMAIL PROTECTED] wrote:


I don't know ... it sound like you are really starting to 
stack up the failures.

I don't know ... I was thinking the other day: what if the 
pilot was pouring a can of Coke into a cup on the flight 
deck and dropped the can and it rolled under the pedals 
and he set his cup down and reached down to pick up the 
can but knocked the yoke which rolled the plane and made 
him push his foot forward and the can got stuck under the 
pedals with the rudder all the way over and the partial 
cup of Coke was knocked over into some electrical stuff 
and shorted it out and killed all the engines on one side 
and the stewardess fell onto the pilot so he couldn't see 
and then ...

Geez, I'm not flying anymore.

;-)

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Re: [Flightgear-devel] [OT] BA-609, V-22 derivative aircraft

2002-12-10 Thread Tony Peden
On Tue, 2002-12-10 at 15:27, Jon S Berndt wrote:
 On 10 Dec 2002 15:18:48 -0800
   Tony Peden [EMAIL PROTECTED] wrote:
 
 I don't know ... it sound like you are really starting to 
 stack up the failures.
 
 I don't know ... I was thinking the other day: what if the 
 pilot was pouring a can of Coke into a cup on the flight 
 deck and dropped the can and it rolled under the pedals 
 and he set his cup down and reached down to pick up the 
 can but knocked the yoke which rolled the plane and made 
 him push his foot forward and the can got stuck under the 
 pedals with the rudder all the way over and the partial 
 cup of Coke was knocked over into some electrical stuff 
 and shorted it out and killed all the engines on one side 
 and the stewardess fell onto the pilot so he couldn't see 
 and then ...
 
 Geez, I'm not flying anymore.
 
 ;-)

Curt, I apologize for even beginning to suggest that you
were stacking things up ...

 
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Re: [Flightgear-devel] [OT] BA-609, V-22 derivative aircraft

2002-12-10 Thread Jon S Berndt
On 10 Dec 2002 15:37:08 -0800
 Tony Peden [EMAIL PROTECTED] wrote:


On Tue, 2002-12-10 at 15:27, Jon S Berndt wrote:


I don't know ... I was thinking the other day: what if the 
...

Curt, I apologize for even beginning to suggest that you
were stacking things up ...


Hey! It could happen!

:-)

Jon

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Re: [Flightgear-devel] [OT] BA-609, V-22 derivative aircraft

2002-12-10 Thread John Check
On Tuesday 10 December 2002 4:22 pm, Curtis L. Olson wrote:

 You could also imagine that something downstream of this central
 transmission could fail, again leaving you in an unhealthy state.  I

unhealthy state you guys crack me up. 
Sounds more like brown trousers time to me ;-)

 agree with the people who are saying this can be made to fly safely
 within reasonable tolerances, but I also think there are certain
 phases where it's probably always going to be a little less safe than
 a helicopter, or perhaps you could say that certain types of failures
 at certain times would be less survivable in the BA-609 ...

 Regards,

 Curt.

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Re: [Flightgear-devel] [OT] BA-609, V-22 derivative aircraft

2002-12-10 Thread Tony Peden
On Tue, 2002-12-10 at 19:24, John Check wrote:
 On Tuesday 10 December 2002 4:22 pm, Curtis L. Olson wrote:
 
  You could also imagine that something downstream of this central
  transmission could fail, again leaving you in an unhealthy state.  I
 
 unhealthy state you guys crack me up. 
 Sounds more like brown trousers time to me ;-)

Fighter pilots do it best, they talk about how a missile could ruin
their whole day.


 
  agree with the people who are saying this can be made to fly safely
  within reasonable tolerances, but I also think there are certain
  phases where it's probably always going to be a little less safe than
  a helicopter, or perhaps you could say that certain types of failures
  at certain times would be less survivable in the BA-609 ...
 
  Regards,
 
  Curt.
 
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