What constrains a paraglider vertically?

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I recently flew on a tandem paraglider for the first time. Since then I keep asking myself a question I have no clear answers to.



While flying I clearly perceived the lift generated by the airfoil, but the strongest feeling I had was as if the paraglider hung to a rail, like a suspension railway, or to a cable, like a cable-car. In other words, I perceived a very strong vertical constraint. I know the airfoil generates lift, but I understand the amount of lift is not enough to give you a stability feeling like when driving a truck! To be similar to the constraint produced by a rail, this vertical constraint should be in the order of thousands of kg, IMHO.



Any suggestions on how to estimate this amount, and its origins?







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  • Let me paraphrase this question a bit: by "constrained", I believe the OP means "very stiff". The acceleration is sudden - e.g. it goes from level flight to ascending flight in a very short amount of time, as opposed to, a general upward acceleration (and associated increase in G loading) lasting for 10 seconds.
    – kevin
    Aug 10 at 2:31














up vote
1
down vote

favorite












I recently flew on a tandem paraglider for the first time. Since then I keep asking myself a question I have no clear answers to.



While flying I clearly perceived the lift generated by the airfoil, but the strongest feeling I had was as if the paraglider hung to a rail, like a suspension railway, or to a cable, like a cable-car. In other words, I perceived a very strong vertical constraint. I know the airfoil generates lift, but I understand the amount of lift is not enough to give you a stability feeling like when driving a truck! To be similar to the constraint produced by a rail, this vertical constraint should be in the order of thousands of kg, IMHO.



Any suggestions on how to estimate this amount, and its origins?







share|improve this question






















  • Let me paraphrase this question a bit: by "constrained", I believe the OP means "very stiff". The acceleration is sudden - e.g. it goes from level flight to ascending flight in a very short amount of time, as opposed to, a general upward acceleration (and associated increase in G loading) lasting for 10 seconds.
    – kevin
    Aug 10 at 2:31












up vote
1
down vote

favorite









up vote
1
down vote

favorite











I recently flew on a tandem paraglider for the first time. Since then I keep asking myself a question I have no clear answers to.



While flying I clearly perceived the lift generated by the airfoil, but the strongest feeling I had was as if the paraglider hung to a rail, like a suspension railway, or to a cable, like a cable-car. In other words, I perceived a very strong vertical constraint. I know the airfoil generates lift, but I understand the amount of lift is not enough to give you a stability feeling like when driving a truck! To be similar to the constraint produced by a rail, this vertical constraint should be in the order of thousands of kg, IMHO.



Any suggestions on how to estimate this amount, and its origins?







share|improve this question














I recently flew on a tandem paraglider for the first time. Since then I keep asking myself a question I have no clear answers to.



While flying I clearly perceived the lift generated by the airfoil, but the strongest feeling I had was as if the paraglider hung to a rail, like a suspension railway, or to a cable, like a cable-car. In other words, I perceived a very strong vertical constraint. I know the airfoil generates lift, but I understand the amount of lift is not enough to give you a stability feeling like when driving a truck! To be similar to the constraint produced by a rail, this vertical constraint should be in the order of thousands of kg, IMHO.



Any suggestions on how to estimate this amount, and its origins?









share|improve this question













share|improve this question




share|improve this question








edited Aug 9 at 21:51









fooot

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asked Aug 8 at 9:33









dtatti

61




61











  • Let me paraphrase this question a bit: by "constrained", I believe the OP means "very stiff". The acceleration is sudden - e.g. it goes from level flight to ascending flight in a very short amount of time, as opposed to, a general upward acceleration (and associated increase in G loading) lasting for 10 seconds.
    – kevin
    Aug 10 at 2:31
















  • Let me paraphrase this question a bit: by "constrained", I believe the OP means "very stiff". The acceleration is sudden - e.g. it goes from level flight to ascending flight in a very short amount of time, as opposed to, a general upward acceleration (and associated increase in G loading) lasting for 10 seconds.
    – kevin
    Aug 10 at 2:31















Let me paraphrase this question a bit: by "constrained", I believe the OP means "very stiff". The acceleration is sudden - e.g. it goes from level flight to ascending flight in a very short amount of time, as opposed to, a general upward acceleration (and associated increase in G loading) lasting for 10 seconds.
– kevin
Aug 10 at 2:31




Let me paraphrase this question a bit: by "constrained", I believe the OP means "very stiff". The acceleration is sudden - e.g. it goes from level flight to ascending flight in a very short amount of time, as opposed to, a general upward acceleration (and associated increase in G loading) lasting for 10 seconds.
– kevin
Aug 10 at 2:31










3 Answers
3






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up vote
5
down vote













What you perceive as "motion" is acceleration.



No acceleration, and you feel no "motion" -- your kinesic sense and inner ear will tell your brain you're sitting still on a solid surface.



What you experienced as "vertical constraint" was nothing more or less than the result of flying in a very stable manner relative to pitch -- no pitching, up or down, means no change in vertical acceleration (which ought to be exactly 1 G at all times, if you're to feel "still"), and no sensation of motion.






share|improve this answer



























    up vote
    4
    down vote














    To be similar to the constraint produced by a rail, this vertical constraint should be in the order of thousands of kg, IMHO. Any suggestions on how to estimate this amount, and its origins?




    The thing is that the constraint is something you "perceived":




    I perceived a very strong vertical constraint




    not that was actually there.



    Only gravity, lift, and drag (and thrust, if powered) are acting on the paraglider, nothing else.



    And the lift is easily estimated, as it is roughly equal to the weight of the passengers and the aircraft summed up and being this a paraglider, definitely not in the range of the thousands of kg.



    Having this been your first experience, the sensation can easily be explained by your lack of familiarity with the transportation method.






    share|improve this answer



























      up vote
      3
      down vote













      Fundamentally, the "constrained" feeling comes from the steepness of the lift coefficient vs angle of attack curve.



      The angle of attack is the angle at which the air approaches the wing. In level flight, this has a certain value, let's say around 5°. Now let's say you encounter a rising pocket of air. Instantaneously, the angle of attack increases. This directly increases the lift coefficient. As a result, the aircraft starts accelerating upwards, until it is ascending as fast as the rising pocket of air, at which point as far as the aircraft is concerned it is in level flight again (while it is in fact rising along with the air pocket). The "sharpness" at which this happens is your "rail-like" feeling of "vertical constraint" as you call it.



      For thin airfoils, the lift coefficient is approximately $2pi alpha$ with $alpha$ the angle of attack. That means that if we were in level flight at $alpha=5°$, we would be accelerating upwards at $1g$ if the angle of attack increased to just 10°. I can promise you that you can't tell such a minute change in the angle of the incoming wind. Therefore, as far as you are concerned, the wind is always coming head on and you feel like you are flying "on rails".



      By the way, "thousands of kilos" of lift for a tandem paraglider of let's say 250kg would mean over $4g$ of acceleration which would be enough to knock you unconscious if sustained for any amount of time.






      share|improve this answer






















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        3 Answers
        3






        active

        oldest

        votes








        3 Answers
        3






        active

        oldest

        votes









        active

        oldest

        votes






        active

        oldest

        votes








        up vote
        5
        down vote













        What you perceive as "motion" is acceleration.



        No acceleration, and you feel no "motion" -- your kinesic sense and inner ear will tell your brain you're sitting still on a solid surface.



        What you experienced as "vertical constraint" was nothing more or less than the result of flying in a very stable manner relative to pitch -- no pitching, up or down, means no change in vertical acceleration (which ought to be exactly 1 G at all times, if you're to feel "still"), and no sensation of motion.






        share|improve this answer
























          up vote
          5
          down vote













          What you perceive as "motion" is acceleration.



          No acceleration, and you feel no "motion" -- your kinesic sense and inner ear will tell your brain you're sitting still on a solid surface.



          What you experienced as "vertical constraint" was nothing more or less than the result of flying in a very stable manner relative to pitch -- no pitching, up or down, means no change in vertical acceleration (which ought to be exactly 1 G at all times, if you're to feel "still"), and no sensation of motion.






          share|improve this answer






















            up vote
            5
            down vote










            up vote
            5
            down vote









            What you perceive as "motion" is acceleration.



            No acceleration, and you feel no "motion" -- your kinesic sense and inner ear will tell your brain you're sitting still on a solid surface.



            What you experienced as "vertical constraint" was nothing more or less than the result of flying in a very stable manner relative to pitch -- no pitching, up or down, means no change in vertical acceleration (which ought to be exactly 1 G at all times, if you're to feel "still"), and no sensation of motion.






            share|improve this answer












            What you perceive as "motion" is acceleration.



            No acceleration, and you feel no "motion" -- your kinesic sense and inner ear will tell your brain you're sitting still on a solid surface.



            What you experienced as "vertical constraint" was nothing more or less than the result of flying in a very stable manner relative to pitch -- no pitching, up or down, means no change in vertical acceleration (which ought to be exactly 1 G at all times, if you're to feel "still"), and no sensation of motion.







            share|improve this answer












            share|improve this answer



            share|improve this answer










            answered Aug 8 at 12:15









            Zeiss Ikon

            8738




            8738




















                up vote
                4
                down vote














                To be similar to the constraint produced by a rail, this vertical constraint should be in the order of thousands of kg, IMHO. Any suggestions on how to estimate this amount, and its origins?




                The thing is that the constraint is something you "perceived":




                I perceived a very strong vertical constraint




                not that was actually there.



                Only gravity, lift, and drag (and thrust, if powered) are acting on the paraglider, nothing else.



                And the lift is easily estimated, as it is roughly equal to the weight of the passengers and the aircraft summed up and being this a paraglider, definitely not in the range of the thousands of kg.



                Having this been your first experience, the sensation can easily be explained by your lack of familiarity with the transportation method.






                share|improve this answer
























                  up vote
                  4
                  down vote














                  To be similar to the constraint produced by a rail, this vertical constraint should be in the order of thousands of kg, IMHO. Any suggestions on how to estimate this amount, and its origins?




                  The thing is that the constraint is something you "perceived":




                  I perceived a very strong vertical constraint




                  not that was actually there.



                  Only gravity, lift, and drag (and thrust, if powered) are acting on the paraglider, nothing else.



                  And the lift is easily estimated, as it is roughly equal to the weight of the passengers and the aircraft summed up and being this a paraglider, definitely not in the range of the thousands of kg.



                  Having this been your first experience, the sensation can easily be explained by your lack of familiarity with the transportation method.






                  share|improve this answer






















                    up vote
                    4
                    down vote










                    up vote
                    4
                    down vote










                    To be similar to the constraint produced by a rail, this vertical constraint should be in the order of thousands of kg, IMHO. Any suggestions on how to estimate this amount, and its origins?




                    The thing is that the constraint is something you "perceived":




                    I perceived a very strong vertical constraint




                    not that was actually there.



                    Only gravity, lift, and drag (and thrust, if powered) are acting on the paraglider, nothing else.



                    And the lift is easily estimated, as it is roughly equal to the weight of the passengers and the aircraft summed up and being this a paraglider, definitely not in the range of the thousands of kg.



                    Having this been your first experience, the sensation can easily be explained by your lack of familiarity with the transportation method.






                    share|improve this answer













                    To be similar to the constraint produced by a rail, this vertical constraint should be in the order of thousands of kg, IMHO. Any suggestions on how to estimate this amount, and its origins?




                    The thing is that the constraint is something you "perceived":




                    I perceived a very strong vertical constraint




                    not that was actually there.



                    Only gravity, lift, and drag (and thrust, if powered) are acting on the paraglider, nothing else.



                    And the lift is easily estimated, as it is roughly equal to the weight of the passengers and the aircraft summed up and being this a paraglider, definitely not in the range of the thousands of kg.



                    Having this been your first experience, the sensation can easily be explained by your lack of familiarity with the transportation method.







                    share|improve this answer












                    share|improve this answer



                    share|improve this answer










                    answered Aug 8 at 10:30









                    Federico♦

                    23.9k1396149




                    23.9k1396149




















                        up vote
                        3
                        down vote













                        Fundamentally, the "constrained" feeling comes from the steepness of the lift coefficient vs angle of attack curve.



                        The angle of attack is the angle at which the air approaches the wing. In level flight, this has a certain value, let's say around 5°. Now let's say you encounter a rising pocket of air. Instantaneously, the angle of attack increases. This directly increases the lift coefficient. As a result, the aircraft starts accelerating upwards, until it is ascending as fast as the rising pocket of air, at which point as far as the aircraft is concerned it is in level flight again (while it is in fact rising along with the air pocket). The "sharpness" at which this happens is your "rail-like" feeling of "vertical constraint" as you call it.



                        For thin airfoils, the lift coefficient is approximately $2pi alpha$ with $alpha$ the angle of attack. That means that if we were in level flight at $alpha=5°$, we would be accelerating upwards at $1g$ if the angle of attack increased to just 10°. I can promise you that you can't tell such a minute change in the angle of the incoming wind. Therefore, as far as you are concerned, the wind is always coming head on and you feel like you are flying "on rails".



                        By the way, "thousands of kilos" of lift for a tandem paraglider of let's say 250kg would mean over $4g$ of acceleration which would be enough to knock you unconscious if sustained for any amount of time.






                        share|improve this answer


























                          up vote
                          3
                          down vote













                          Fundamentally, the "constrained" feeling comes from the steepness of the lift coefficient vs angle of attack curve.



                          The angle of attack is the angle at which the air approaches the wing. In level flight, this has a certain value, let's say around 5°. Now let's say you encounter a rising pocket of air. Instantaneously, the angle of attack increases. This directly increases the lift coefficient. As a result, the aircraft starts accelerating upwards, until it is ascending as fast as the rising pocket of air, at which point as far as the aircraft is concerned it is in level flight again (while it is in fact rising along with the air pocket). The "sharpness" at which this happens is your "rail-like" feeling of "vertical constraint" as you call it.



                          For thin airfoils, the lift coefficient is approximately $2pi alpha$ with $alpha$ the angle of attack. That means that if we were in level flight at $alpha=5°$, we would be accelerating upwards at $1g$ if the angle of attack increased to just 10°. I can promise you that you can't tell such a minute change in the angle of the incoming wind. Therefore, as far as you are concerned, the wind is always coming head on and you feel like you are flying "on rails".



                          By the way, "thousands of kilos" of lift for a tandem paraglider of let's say 250kg would mean over $4g$ of acceleration which would be enough to knock you unconscious if sustained for any amount of time.






                          share|improve this answer
























                            up vote
                            3
                            down vote










                            up vote
                            3
                            down vote









                            Fundamentally, the "constrained" feeling comes from the steepness of the lift coefficient vs angle of attack curve.



                            The angle of attack is the angle at which the air approaches the wing. In level flight, this has a certain value, let's say around 5°. Now let's say you encounter a rising pocket of air. Instantaneously, the angle of attack increases. This directly increases the lift coefficient. As a result, the aircraft starts accelerating upwards, until it is ascending as fast as the rising pocket of air, at which point as far as the aircraft is concerned it is in level flight again (while it is in fact rising along with the air pocket). The "sharpness" at which this happens is your "rail-like" feeling of "vertical constraint" as you call it.



                            For thin airfoils, the lift coefficient is approximately $2pi alpha$ with $alpha$ the angle of attack. That means that if we were in level flight at $alpha=5°$, we would be accelerating upwards at $1g$ if the angle of attack increased to just 10°. I can promise you that you can't tell such a minute change in the angle of the incoming wind. Therefore, as far as you are concerned, the wind is always coming head on and you feel like you are flying "on rails".



                            By the way, "thousands of kilos" of lift for a tandem paraglider of let's say 250kg would mean over $4g$ of acceleration which would be enough to knock you unconscious if sustained for any amount of time.






                            share|improve this answer














                            Fundamentally, the "constrained" feeling comes from the steepness of the lift coefficient vs angle of attack curve.



                            The angle of attack is the angle at which the air approaches the wing. In level flight, this has a certain value, let's say around 5°. Now let's say you encounter a rising pocket of air. Instantaneously, the angle of attack increases. This directly increases the lift coefficient. As a result, the aircraft starts accelerating upwards, until it is ascending as fast as the rising pocket of air, at which point as far as the aircraft is concerned it is in level flight again (while it is in fact rising along with the air pocket). The "sharpness" at which this happens is your "rail-like" feeling of "vertical constraint" as you call it.



                            For thin airfoils, the lift coefficient is approximately $2pi alpha$ with $alpha$ the angle of attack. That means that if we were in level flight at $alpha=5°$, we would be accelerating upwards at $1g$ if the angle of attack increased to just 10°. I can promise you that you can't tell such a minute change in the angle of the incoming wind. Therefore, as far as you are concerned, the wind is always coming head on and you feel like you are flying "on rails".



                            By the way, "thousands of kilos" of lift for a tandem paraglider of let's say 250kg would mean over $4g$ of acceleration which would be enough to knock you unconscious if sustained for any amount of time.







                            share|improve this answer














                            share|improve this answer



                            share|improve this answer








                            edited Aug 9 at 21:14

























                            answered Aug 8 at 13:59









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