Welcome to Flightinfo.com

  • Register now and join the discussion
  • Friendliest aviation Ccmmunity on the web
  • Modern site for PC's, Phones, Tablets - no 3rd party apps required
  • Ask questions, help others, promote aviation
  • Share the passion for aviation
  • Invite everyone to Flightinfo.com and let's have fun

Free-fall Autorotate?

Welcome to Flightinfo.com

  • Register now and join the discussion
  • Modern secure site, no 3rd party apps required
  • Invite your friends
  • Share the passion of aviation
  • Friendliest aviation community on the web
Actually, the torque from the autorotating main rotor feeds back into the main transmission, and the friction in the drivetrain actually drives the airframe out of balance in the opposite direction from powered flight. To stay in trimmed flight and reduce your rate of descent, you have to feed in opposite pedal. It happens pretty naturally, the pilot is going to trim to balanced flight as a matter of habit, but there is a pedal input required.
I guess so. Geez its been so long that I'd forgotten!
 
I have not seen the movie but do not think it is feasible. Lift is keeping the helicopter upright in flight. Without it, it is a rock with nothing providing a stablizing force for a pilot to use in keeping it upright.

As far as the NOTAR goes; the slot that runs along side the tailboom is called a Coanda slot. There was supposed to be a fan off the transmission that provided 15psi or so of pressure out the side of this slot that would provide a counter torque effect in conjunction with the downwash created by the main rotar that would increase/decrease static and dynamic pressure and make it work well, in flight, as an antitorque force. However, one of the weaknesses that was found was the ability of the downwash to provide this differential pressure in an autorotation. In an autorotation the helicopter roter blade is free wheeling (sprag clutch) and it is not creating a downwash in an autorotation. The Coanda slot wasn't providing enough antitorque capability and they were having control problems with it. So they decided to go to the H or V style stabilator and apparantly it was working better. However, I still heard there are some problems with it when you load the aircraft and perform the same manuevers. Not only control issues but power issues as well.

I have alot of Army helicopter time but never flew the NOTAR (No Tail Rotor). It was supposed to be so easy to fly that the FAA was considering making it a different rating altogether. Not sure if it ever went through or not.

Even James Bond couldn't make that stunt work. I would bet money if anyone could do it, the little bird drivers of the 160th Night Stalkers could. If they couldn't do it, NO ONE could.

Just my .02. Helicopters kick ASS!!!!
 
I understand your humble opinion Matt but you also said "Aside from the fact you would disintegrate into a massive mess of metal and plastic when falling vertically with no Nr." and that is unlikely to happen until it hits the ground.

Let's go smaller scale, and we won't even use a cat. Have you ever seen a parachutist jump out of an airplane wearing a snowboard? Or have you ever seen them drop a car out? In the case of the snowboard, the parachutist is automatically pushed underneath the large flat panel of the snowboard and he hangs very stable underneath it. He isn't even a cat!!! When they drop a car out, it is also a very flat surface and it often stabilizes in the air. Many times the car will remain stable for a very long time. Look at some of the vidoes on youtube. Sometimes the car rolls. That is why I say it is feasible.

There is a lot of potential that it could happen. on many rotor systems you can get the rotor to spool up almost instantaneously during an autorotation so I have no doubt given enough time the blades would spin fast enough. There is also more potential that you could start a helicopter in the air even if it is not wings level or even upright as it is falling allowing the rotors to spool up. Turbine engines don't care what direction they are facing when you start them unless of course you are ramming about 120 kts of wind in from the back which of course could hapen.

So I still say it is feasible as the large surface area of the rotors would act like out riggers as the aircraft fell stabilizing it in the process. I am not saying it would work every time or even most times but it is plausible that it could work.

Remember, the laws of physics say a bee cannot fly.

I've flown helicopters for 18 years, hold a degree in aeronautics and am currently staying at a holiday in express!! Actually I am in the BOQ at ATC but its just as good. So there.

Of course now that you deleted your post none of this post especially the smarmy experience comment makes sense to anyone else as it related to items in your post. Just great!
 
Last edited:
I lost faith in Mythbusters when it comes to anything aviation related when they tried to prove whether an airplane would take off if it was on a treadmill going the same speed and in theory keeping the aircraft stationary.

The answer is obviously no as it doesn't matter how fast the wheels are turning, it matters how fast the plane is moving so that lift is created over the wings. If the plane is stationary, there is no lift. Anyway, they declared it plausible despite a poorly designed test bed.

So if they can't do that simple test, I would hate to see what they would do with this.
 
Some RC heli guys are doing blade-stop autorotations now. If they wait too long to get the blades going after they stop, and it doesn't take much, the heli will tumble out of control and then it's all over.
 
In defense of Mythbusters, that prop-driven "jetpack" very nearly left the ground. Maybe if they inhaled enough helium......
 
I lost faith in Mythbusters when it comes to anything aviation related when they tried to prove whether an airplane would take off if it was on a treadmill going the same speed and in theory keeping the aircraft stationary.

The answer is obviously no as it doesn't matter how fast the wheels are turning, it matters how fast the plane is moving so that lift is created over the wings. If the plane is stationary, there is no lift. Anyway, they declared it plausible despite a poorly designed test bed.

So if they can't do that simple test, I would hate to see what they would do with this.

Of course the airplane wouldn't fly without airspeed. Nobody but a moron would argue otherwise. But the whole point is that the treadmill can't stop the plane from moving.

What test bed would you propose?

It's a flawed question.
 
What test bed would you propose?

It's a flawed question.

Here is the question posed in one spot:

"A plane is standing on a large treadmill or conveyor belt. The plane moves in one direction, while the conveyor moves in the opposite direction. This conveyor has a control system that tracks the plane speed and tunes the speed of the conveyor to be exactly the same (but in the opposite direction). Can the plane take off?"

Here it is posed a bit differently somewhere else:

"Imagine a 747 is sitting on a conveyor belt, as wide and long as a runway. The conveyor belt is designed to exactly match the speed of the wheels, moving in the opposite direction. Can the plane take off?"


You are absolutely right it is a flawed question and one that has two answers depending exactly how one looks at it. If the wheels and the treadmill are going the exact speed as posed in the first part of the question, then the answer is no it cannot takeoff, as the plane is obviously not moving forward. But if the question is "can the plane overcome the force of the treadmill, move forward and take off," the answer is yes because the plane's thrust can easily push past the minimal friction caused by the treadmill on the wheels since the wheels don't drive the airplane. That is why an airplane can take of on ice easily. But for this to be true the wheels on the aircraft are moving faster than the treadmill (or else there is no forward motion) so the wheels and the treadmill are no longer equal.

That is why I lost faith in their experiment. They only looked at one point of view despite the fact that the question was flawed.

Now back to our physics/bad guy defying question.
 
Last edited:
Now back to our physics/bad guy defying question.

Allright, anybody wanna design and build a rotor-wing glider? Paging Otto Sikorsky...

Just make sure they stay in high tow...
 
I thought about that but the rotor blades normally cone when a large collective load is applied. If the aircraft is flat pitch, I agree that they will cone up but depending on the rotor system, fully articulated vs rigid vs whatever else, they may not cone to the point where they would break since they are in free fall and not working to lift the helicopter.

There is no science to these ramblings by the way, just thoughts.
 

Latest resources

Back
Top Bottom