- Joined
- May 7, 2011
- Messages
- 90
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Hi all,
Can someone please explain to me the concept behind the turbo solution. I get that instead of using the quadratric equation, we can use a short cut. I get why we are using the formula v0/g and get 26.8 for the upward flight but I don't understand why we can't add 2.8 seconds plus 2.8 seconds to get the total flight time when it reaches the ground, this way we can just plug in into the x direction equation which is x= vxt .
If they just added the other flight time using d= voyt + 1/2 at^2 then why didn't they add the initial velocity 26.8 in order to find the other time flight that it takes to get down if this is the displacement equation and velocity is giving in the y direction. I guess I'm confused why the initial velocity in the the y direction is not added to their turbo shorcut if you need the velocity in the y direction. Help please !
Can someone please explain to me the concept behind the turbo solution. I get that instead of using the quadratric equation, we can use a short cut. I get why we are using the formula v0/g and get 26.8 for the upward flight but I don't understand why we can't add 2.8 seconds plus 2.8 seconds to get the total flight time when it reaches the ground, this way we can just plug in into the x direction equation which is x= vxt .
If they just added the other flight time using d= voyt + 1/2 at^2 then why didn't they add the initial velocity 26.8 in order to find the other time flight that it takes to get down if this is the displacement equation and velocity is giving in the y direction. I guess I'm confused why the initial velocity in the the y direction is not added to their turbo shorcut if you need the velocity in the y direction. Help please !