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 » Soaring
Site Map Home Register Authors List Search Today's Posts Mark Forums Read Web Partners

Safety of winch launch vrs. aero tow?



 
 
Thread Tools Display Modes
  #1  
Old October 29th 03, 08:38 PM
Bob Johnson
external usenet poster
 
Posts: n/a
Default

As long as we're sitting around the campfire and also to show you I can
go both ways, I 'member a time only a couple of years ago that I
experienced the dreaded aerotow line break at 200 ft and 60 kt over the
outbound fence.

I looked out front and it wasn't too exiting, so I gingerly turned
ninety to the left and the scenery looked some better, but not the
greatest, so I REALlY gingerly gave it another ninety to the left and
was really impressed this time as I found I was perfectly lined up with
the takeoff runway. And I recall I hadn't lost too much of my original
60 kt. Will wonders never cease!!

I thought "OK now God, you've made it possible for me to do this little
magic trick perfectly the first time I tried it in front of all my
friends and hangar bums, give me your hand again and let's try just one
more."

So I pulled spoilers, checked gear down and rolled up to my exact
takeoff spot.

And as I popped the canopy, my good friend who shall remain nameless,
said "S--t!, you've gone and lost us another Tost ring, somebody go back
to the hangar and see if they can find another tow rope". It was his
turn to tow, so I pushed back. Nobody else said a word.

Safety lecture from a dummy follows:

I don't remember to this day why I ninetied to the left. During the
previous year's biannual when Juan Batch pulled the plug on me over his
outbound fence, turning right was the correct choice because in that
direction lay the wind, which blows one back over the airport. This
improves the scenery like you wouldn't believe.

When I tried the trick for real solo, the wind lay to my left. I'd like
to think it was instinct. But I believe it was a coin toss.

Anyway, thank God. And Juan.

It Depends

BJ






Bob Johnson wrote:

Hi Bill --

I 'member my O-Nine Two oil field piano wire breaking at the half way
point during a tow in Roy Schlemeyer's old SGS 2-22. I yelled "Oh, line
break" or something to that effect and recall the glider innards debris
collected since the last ice age floating up and dancing before my eyes
as I dumped the stick full forward. Was it half a second before I
reacted? Can't believe I waited that long. And when the astronauts tell
you that zero-g is exhilarating, believe it.

Luckily, I had been well briefed by Roy as to what to expect. It has
been theorized that some people are "allergic" to zero-g and they
instinctively jerk the stick full back instead of push full forward.
Unfortunately, this is the last mistake they ever make and we can no
longer interview them as to why they did this.

There, we're back to the original question, "Is winch launch safer than
aerotow?" The answer? -- scroll down

IT DEPENDS!

Thanks and good to hear from you again.

BJ



Bill Daniels wrote:

"Bob Johnson" wrote in message
...
Eggert --

Those are really good numbers for your winch.

With V8 300 HP (GMC 454 c.i., 7.4 L), and 5000 ft (1550 m) Plasma line
laid out, we are getting the rule of thumb 1/3 cable length releases of
1700 ft (525 m). This is into 10-15 kt wind. Much over that, we leave
the Blanik in the barn!

BJ
Midland, Texas


Bob, When winching, the wind is your friend. Quitting at 15 knots is not
necessary. I have winched into 35 knots and higher winds and the results
are spectacular. Each 10 knots of headwind is the equivalent of about 40
additional HP.

The thing that often severely limits the altitude gained is a slow pitch-up
profile at the start of the launch. The final height achieved is largely
determined by the profile flown in the first few seconds of the launch.

Now, as everyone has pointed out, you need to be careful here. Safety at
the start of the climb is a combination of airspeed, altitude and attitude.
The more you have of the first, the faster you can get the second two and
the higher you will get.

I've done calculations, simulator runs (X-Plane) and flight test to prove
the following point. If you have 60 knots in a glider with a stalling
airspeed of 40 knots, you can be in full climb attitude at zero altitude and
still have a large safety margin. Practice this way - at several thousand
feet AGL, zoom the glider into a 50 degree nose-up attitude. As the
airspeed decays to 60 knots, yell "WIRE BREAK", delay 0.5 seconds
(simulating reaction time) and pitch forward at zero G. Watch the airspeed
and altitude, you'll see what I mean. (For winch CFI-G's, this is a great
way to teach how to handle wire breaks.)

If you have (or simulate) a wire break at this point and start a zero G
pitch over after a .5 second delay, the minimum airspeed during the
parabolic ballistic trajectory will be about 50 - 55 knots when the glider
reaches apogee at an altitude of about 100 feet AGL. So there you are at
100 feet and 55 knots in a normal gliding attitude - not exactly a
problematic situation, just land straight ahead. The reason this works is
that the glider's induced drag at zero G is minimal so the airspeed decay is
mainly just due to gravity and the glider follows a parabolic trajectory
until the pilot re-establishes one G at the normal glide attitude.

I need to repeat that I am not advocating a rocket blast-off kind of climb
profile but a smooth transition into the full climb without undue delay
equipped with a full understanding of the safety margins.

Bill Daniels

  #2  
Old October 30th 03, 10:11 AM
Robert Ehrlich
external usenet poster
 
Posts: n/a
Default

Bob Johnson wrote:

As long as we're sitting around the campfire and also to show you I can
go both ways, I 'member a time only a couple of years ago that I
experienced the dreaded aerotow line break at 200 ft and 60 kt over the
outbound fence.

I looked out front and it wasn't too exiting, so I gingerly turned
ninety to the left and the scenery looked some better, but not the
greatest, so I REALlY gingerly gave it another ninety to the left and
was really impressed this time as I found I was perfectly lined up with
the takeoff runway. And I recall I hadn't lost too much of my original
60 kt. Will wonders never cease!!

I thought "OK now God, you've made it possible for me to do this little
magic trick perfectly the first time I tried it in front of all my
friends and hangar bums, give me your hand again and let's try just one
more."

So I pulled spoilers, checked gear down and rolled up to my exact
takeoff spot.

And as I popped the canopy, my good friend who shall remain nameless,
said "S--t!, you've gone and lost us another Tost ring, somebody go back
to the hangar and see if they can find another tow rope". It was his
turn to tow, so I pushed back. Nobody else said a word.

Safety lecture from a dummy follows:

I don't remember to this day why I ninetied to the left. During the
previous year's biannual when Juan Batch pulled the plug on me over his
outbound fence, turning right was the correct choice because in that
direction lay the wind, which blows one back over the airport. This
improves the scenery like you wouldn't believe.

When I tried the trick for real solo, the wind lay to my left. I'd like
to think it was instinct. But I believe it was a coin toss.

Anyway, thank God. And Juan.

It Depends

BJ


This raises the interesting question of the height loss during a 180 degrees
turn in a glider or an airplane with a dead engine. I recently had a dicsussion
about that with a friend who is a power pilot and on this occasion made again a
small computation I had already made on this matter. As I never have seen
these results elsewhere, I think it may useful to show that here. Assume
you fly your turn wit an angle of attack which correspond to the speed V
when flying straight and wings level, and that the vertical sink speed
in the same conditions wuold be Vz, then during this 180 degrees turn
flown with a bank angle phi, the height loss is pi*V*Vz/(g*sin(phi)*cos(phi)),
and the turn is flown at speed V/sqrt(cos(phi)). The optimum (minimal
height loss) is when sin(phi)*cos(phi) is maximum, i.e. phi = 45 degrees,
and the product V*Vz is minimum. A glance on a typical glider polar will
show that this last thing is obtained with V just below min sink speed, but
as it is not easy to find how many below, let's assume the turn is done
at min sink speed, this is not very far from the optimum. For a typical
glider with min sink of .6 m/s at 80 km/h (22.2 m/s) the height loss is
8.5 m, for a typical airplane with min sink of 3 m/s at 120 km/h (33.3 m/s)
the height loss is 64 m. This explains why the 180 degrees turn back to
the runway over the outbound fence succeeds in a glider but not in a power
plane.

In the case mentioned above, the speed (60kt) was far over the optimum,
however the result is as expected not catastrophic. Assuming a bank angle
of 45 degrees, the equivalent speed in straight flight would be multiplied
by 1.18, this gives 26 m/s or 93 km/h. Assuming the sink speed is 1 m/s in these
conditions, we get a height loss of 16.6m. This is for a poor glider (L/D =
26 at 93 km/h).
  #3  
Old October 30th 03, 01:50 PM
Martin Gregorie
external usenet poster
 
Posts: n/a
Default

On Thu, 30 Oct 2003 10:11:18 +0000, Robert Ehrlich
wrote:

Bob Johnson wrote:

As long as we're sitting around the campfire and also to show you I can
go both ways, I 'member a time only a couple of years ago that I
experienced the dreaded aerotow line break at 200 ft and 60 kt over the
outbound fence.

I looked out front and it wasn't too exiting, so I gingerly turned
ninety to the left and the scenery looked some better, but not the
greatest, so I REALlY gingerly gave it another ninety to the left and
was really impressed this time as I found I was perfectly lined up with
the takeoff runway. And I recall I hadn't lost too much of my original
60 kt. Will wonders never cease!!

I thought "OK now God, you've made it possible for me to do this little
magic trick perfectly the first time I tried it in front of all my
friends and hangar bums, give me your hand again and let's try just one
more."

So I pulled spoilers, checked gear down and rolled up to my exact
takeoff spot.

And as I popped the canopy, my good friend who shall remain nameless,
said "S--t!, you've gone and lost us another Tost ring, somebody go back
to the hangar and see if they can find another tow rope". It was his
turn to tow, so I pushed back. Nobody else said a word.

Safety lecture from a dummy follows:

I don't remember to this day why I ninetied to the left. During the
previous year's biannual when Juan Batch pulled the plug on me over his
outbound fence, turning right was the correct choice because in that
direction lay the wind, which blows one back over the airport. This
improves the scenery like you wouldn't believe.

When I tried the trick for real solo, the wind lay to my left. I'd like
to think it was instinct. But I believe it was a coin toss.

Anyway, thank God. And Juan.

It Depends

BJ


This raises the interesting question of the height loss during a 180 degrees
turn in a glider or an airplane with a dead engine. I recently had a dicsussion
about that with a friend who is a power pilot and on this occasion made again a
small computation I had already made on this matter. As I never have seen
these results elsewhere, I think it may useful to show that here. Assume
you fly your turn wit an angle of attack which correspond to the speed V
when flying straight and wings level, and that the vertical sink speed
in the same conditions wuold be Vz, then during this 180 degrees turn
flown with a bank angle phi, the height loss is pi*V*Vz/(g*sin(phi)*cos(phi)),
and the turn is flown at speed V/sqrt(cos(phi)). The optimum (minimal
height loss) is when sin(phi)*cos(phi) is maximum, i.e. phi = 45 degrees,
and the product V*Vz is minimum. A glance on a typical glider polar will
show that this last thing is obtained with V just below min sink speed, but
as it is not easy to find how many below, let's assume the turn is done
at min sink speed, this is not very far from the optimum. For a typical
glider with min sink of .6 m/s at 80 km/h (22.2 m/s) the height loss is
8.5 m, for a typical airplane with min sink of 3 m/s at 120 km/h (33.3 m/s)
the height loss is 64 m. This explains why the 180 degrees turn back to
the runway over the outbound fence succeeds in a glider but not in a power
plane.

In the case mentioned above, the speed (60kt) was far over the optimum,
however the result is as expected not catastrophic. Assuming a bank angle
of 45 degrees, the equivalent speed in straight flight would be multiplied
by 1.18, this gives 26 m/s or 93 km/h. Assuming the sink speed is 1 m/s in these
conditions, we get a height loss of 16.6m. This is for a poor glider (L/D =
26 at 93 km/h).


Thanks for that. A most informative calculation and certainly matches
my most recent relevant experience.

The last time I was having a supervised aero-tow refresher in our
Puchacz I was doing a running commentary for the instructors benefit
and as soon as I said "400 ft - no problem now from a rope break" BANG
as he pulled the release. We had a touch over 60 kts and as soon as I
saw the rope go I pulled a 45 degree banked 180, keeping the 60 kts
just as Bob described, and was amazed at how easily we got in over the
fence. In fact, once I'd rolled out it looked like a normal approach,
so I opened the brakes and did a typical Puchacz approach and landing.

--
martin@ : Martin Gregorie
gregorie : Harlow, UK
demon :
co : Zappa fan & glider pilot
uk :

  #4  
Old October 30th 03, 07:49 PM
Jack
external usenet poster
 
Posts: n/a
Default

in article , Robert Ehrlich at
wrote on 2003/10/30 4:11:

Bob Johnson wrote:


I 'member a time only a couple of years ago that I experienced the
dreaded aerotow line break at 200 ft and 60 kt over the...fence.


This raises the interesting question of the height loss during a 180
degree turn in a glider or an airplane with a dead engine.


The considerations are not so different for a power plane or a glider, but
the parameters are different. See the cites/sites below in their entirety at
the inlcuded URLs for the discussion as applied to Genral Aviation ASEL
types:

--------------------

Should You Turnback?
or
The Possible `Impossible' Turn
by
David F. Rogers, PhD

Copyright (C) 1991 by David F. Rogers. All rights reserved.


"Most of us fly single engine aircraft. If the engine quits
on takeoff, should you attempt to turnback to land on the
runway? The turnback problem is extremely complex. Like many
complex problems, there is no single right answer. Each
situation must be judged individually. Thus, the answer is
a qualified maybe or the classical `it depends'. It depends
on the Conditions, the Aircraft, the Altitude, the
Proficiency of the pilot and on Planning. CAAPP for short."

http://web.usna.navy.mil/~dfr/flying/possible.html

================================================== ==========

The Possible `Impossible' Turn

David F. Rogers
United States Naval Academy
Annapolis, Maryland 21402

Copyright 1994 David F. Rogers, All rights reserved.
Originally published in the AIAA Journal of Aircraft, Vol. 32,
pp. 392-397, 1995 with permission.

"Turning back after engine failure during the take-off phase
of flight in a single engine aircraft is examined using a
simplified analytical model. The important parameters are
identified. The analysis shows that the optimum flight path
is teardrop shaped with a 45-degree bank angle at stall
velocity during the turn. The effects of engine failure
altitude, wind direction and velocity, and bank angle on
the required runway length are examined. The results show
that the typical recommendations for general aviation
single engine aircraft are not optimum."

http://web.usna.navy.mil/~dfr/flying/aiaa1col.pdf

================================================== ==========

  #5  
Old November 3rd 03, 05:28 AM
Mark James Boyd
external usenet poster
 
Posts: n/a
Default

In power planes I often wondered how high I would need to turn around,
and the biggest difference seemed to be how well I was climbing.
In a heavy Piper Arrow on a hot day, We couldn't climb fast enough
to ever glide back regardless how high we went if we did a
straight out or 45 departure. Departing downwind was another story,
of course.

On hot days with heavy loads at Avenal, the tug sometimes turns very
gently at low altitudes to downwind. I recall flying a two seater open
cockpit on a very hot day and seeing miserable climb out of us
and the 150/150. In our case not a problem with all the
flat ground, but still a bit disconcerting to be
so far out and low...

  #6  
Old November 3rd 03, 03:52 PM
Bill Daniels
external usenet poster
 
Posts: n/a
Default


"Mark James Boyd" wrote in message
news:3fa5f571$1@darkstar...
In power planes I often wondered how high I would need to turn around,
and the biggest difference seemed to be how well I was climbing.
In a heavy Piper Arrow on a hot day, We couldn't climb fast enough
to ever glide back regardless how high we went if we did a
straight out or 45 departure. Departing downwind was another story,
of course.

On hot days with heavy loads at Avenal, the tug sometimes turns very
gently at low altitudes to downwind. I recall flying a two seater open
cockpit on a very hot day and seeing miserable climb out of us
and the 150/150. In our case not a problem with all the
flat ground, but still a bit disconcerting to be
so far out and low...


Back in around 1970 a power instructor who had witnessed glider 200 foot 180
turns back to the runway wanted to try some in a Cessna 150. I rode with
him as we tried a few at a safe altitude. The 150 was one of the old ones
with a straight tail and manual flaps.

The glider technique of a 45 degree banked turn was very marginal. We then
experimented with some more aggressive maneuvers. The best seem to be a
sort of diving 180 degree rolling turn with a pullout from the dive on the
reciprocal heading. We came out of the dive headed towards the runway at
high airspeed but in ground effect which got us to the runway with ease.

Once we were confident of our technique, we tried a few at Caddo Mills, TX.
At the time, Caddo Mills was just abandoned runways with no buildings or
fences and surrounded by alfalfa fields. The 45 degree turn never made it
back but the diving roll did work if you were quick and aggressive.

We both agreed that the conventional instruction of not trying a 180 below
about 500 feet was best.

Bill Daniels

  #7  
Old November 3rd 03, 10:41 PM
Colin
external usenet poster
 
Posts: n/a
Default

"Bill Daniels" wrote:


"Mark James Boyd" wrote in message
news:3fa5f571$1@darkstar...
In power planes I often wondered how high I would need to turn around,
and the biggest difference seemed to be how well I was climbing.
In a heavy Piper Arrow on a hot day, We couldn't climb fast enough
to ever glide back regardless how high we went if we did a
straight out or 45 departure. Departing downwind was another story,
of course.

On hot days with heavy loads at Avenal, the tug sometimes turns very
gently at low altitudes to downwind. I recall flying a two seater open
cockpit on a very hot day and seeing miserable climb out of us
and the 150/150. In our case not a problem with all the
flat ground, but still a bit disconcerting to be
so far out and low...


Back in around 1970 a power instructor who had witnessed glider 200 foot 180
turns back to the runway wanted to try some in a Cessna 150. I rode with
him as we tried a few at a safe altitude. The 150 was one of the old ones
with a straight tail and manual flaps.

The glider technique of a 45 degree banked turn was very marginal. We then
experimented with some more aggressive maneuvers. The best seem to be a
sort of diving 180 degree rolling turn with a pullout from the dive on the
reciprocal heading. We came out of the dive headed towards the runway at
high airspeed but in ground effect which got us to the runway with ease.

Once we were confident of our technique, we tried a few at Caddo Mills, TX.
At the time, Caddo Mills was just abandoned runways with no buildings or
fences and surrounded by alfalfa fields. The 45 degree turn never made it
back but the diving roll did work if you were quick and aggressive.

We both agreed that the conventional instruction of not trying a 180 below
about 500 feet was best.

Bill Daniels


Many years ago a highly respected aerobatic pilot in UK (still working
today) wrote an article in our Pilot magazine on this subject. He
reminded us that three things were required:
1. A rapid 180 degree change of heading.
2. Minimum loss of height.
3. Normal airspeed at the end of the manoever.
Controversially, he maintained that a highly banked slipping turn
satisfies all three criteria. The rate of decent is very high during
the turn, but the duration is so short that it results in less height
loss than either of the two alternatives (eg:slow and gentle or fast
and furious), and the airspeed is normal throughout.
Just don't forget to keep loads of top rudder on.

- Colin

  #8  
Old November 4th 03, 10:49 AM
Robert Ehrlich
external usenet poster
 
Posts: n/a
Default

Colin wrote:

Many years ago a highly respected aerobatic pilot in UK (still working
today) wrote an article in our Pilot magazine on this subject. He
reminded us that three things were required:
1. A rapid 180 degree change of heading.
2. Minimum loss of height.
3. Normal airspeed at the end of the manoever.
Controversially, he maintained that a highly banked slipping turn
satisfies all three criteria. The rate of decent is very high during
the turn, but the duration is so short that it results in less height
loss than either of the two alternatives (eg:slow and gentle or fast
and furious), and the airspeed is normal throughout.
Just don't forget to keep loads of top rudder on.

- Colin



I don't see why the turn should be a slipping one, you certainly will
loose more height in a slipping turn than in a normal one. And height
loss is what make the turn possible or not.
 




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
Parachute fails to save SR-22 Capt.Doug Piloting 72 February 10th 05 05:14 AM
spaceship one Pianome Home Built 169 June 30th 04 05:47 AM
The Internet public meeting on National Air Tour Standards begins Feb. 23 at 9 a.m. Larry Dighera Piloting 0 February 22nd 04 03:58 PM
USAF = US Amphetamine Fools RT Military Aviation 104 September 25th 03 03:17 PM
using winch instead of aerotow goneill Soaring 5 August 27th 03 02:46 PM


All times are GMT +1. The time now is 03:10 PM.


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