Finding the terminal velocity of a model rocket from a list of velocities

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The discussion revolves around analyzing rocket data from a 20,000-foot launch to calculate terminal velocity and the drag coefficient. The user has time, altitude, and velocity data but struggles to graph the velocities effectively to identify terminal velocity. Suggestions include using Excel to calculate velocity as a function of height and focusing on the data from burnout to apogee, as drag coefficients differ during ascent and descent. There is a consensus that while calculating terminal velocity during coasting is challenging, it may be possible to estimate an upper bound for free fall terminal velocity. The user aims to validate the drag coefficient, which is typically around 0.75 but varies with different rocket designs.
  • #91
erobz said:
move the formula down one cell. Then just stop it at the end. you are going to truncate the data a bit more to remove some outliers, or you could remove them point by point if you feel like it.
here is what i have for beta, using avg acel for dv/dt. B=(-ma-mg)/v^2

the numbers are odd, and when i plot it.... man it looks nasty
1677686655169.png
 
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  • #92
erobz said:
I want you to take the average acceleration across each time step (just for the truncated data).

##a_{avg} = \frac{ v_2 - v_1 }{ t_2- t_1}##

and arithmetic average velocity over the same time step

## v_{avg} = \frac{v_1 + v_2}{2}##

You are then going to plot ##\beta## vs ##v_{avg}##
This is the exact trick we used in atmospheric modeling to determine the final steady state ozone column without running the calculation out to infinite time.
 
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  • #93
Chestermiller said:
This is the exact trick we used in atmospheric modeling to determine the final steady state ozone column without running the calculation out to infinite time.
thats cool. Its been great the last couple of days with this personal challenge of mine. This entire question is not for an assignment, but for my understanding and growth. I am so used to bookwork and homework questions, that i decided to branch out and ask myself how i would do this. I will USE this data though in my senior capstone report.
 
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  • #94
LT72884 said:
here is what i have for beta, using avg acel for dv/dt. B=(-ma-mg)/v^2

the numbers are odd, and when i plot it.... man it looks nasty
View attachment 323047
##a_{avg}## is negative. The acceleration of the rocket is opposite its direction of motion. What you have is positive. What calculation did you do for that? After you fix it, please share the plot so we can try to interpret it. Or maybe you can offer you interpretation of it... more than the "numbers are odd, and it looks nasty", think about if its average behavior aligns with any expectations about ##\beta##.
 
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  • #95
erobz said:
##a_{avg}## is negative. The acceleration of the rocket is opposite its direction of motion. What you have is positive. What calculation did you do for that? After you fix it, please share the plot so we can try to interpret it. Or maybe you can offer you interpretation of it... more than the "numbers are odd, and it looks nasty", think about if its average behavior aligns with any expectations about ##\beta##.
i used a=(v2-v1)/(t2-t1) but if it needs to be -, then i will switch it around
1677693457865.png
 
  • #96
LT72884 said:
i used a=(v2-v1)/(t2-t1) but if it needs to be -, then i will switch it around
View attachment 323051
If you did use that formula you would be getting a negative value, and you aren't.
 
  • #97
erobz said:
If you did use that formula you would be getting a negative value, and you aren't.
exactly. But excel shows that i am using the correct formula. Ill just reverse the C3 and C2 values, that will produce negative numbers. I just dont know if beta is correct.
if i let B=(rho)(Cd)(Ar)(0.5) and solve for cd, i get 0.72 for the first entry. Now, Cd does change ALOT during a flight due to many factors. So a plot of Beta should look almost like a switch back type trail..

1677694033074.png
 
  • #98
if i did indeed solve for the Cd correctly, i can use that in the terminal velocity equation by taking the average Cd over a specific time. When velocity is 0.3m/s my drag coef is -44,000 so its gotta be the right numbers.

or did you have a different aproach to find Tv?
 
  • #99
LT72884 said:
if i did indeed solve for the Cd correctly, i can use that in the terminal velocity equation by taking the average Cd over a specific time. When velocity is 0.3m/s my drag coef is -44,000 so its gotta be the right numbers.

or did you have a different aproach to find Tv?
Well, you need to solve for the drag coefficient ##C_d## from ##\beta##. What do you calculate as ##\beta##, how did you get it? Please elaborate on what you are doing to get these numbers. Can you please share the plot? I think the variation you are seeing is noise, not the variation of ##\beta## as a function of ##v_{avg}##.
 
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  • #100
erobz said:
Well, you need to solve for the drag coefficient ##C_d## from ##\beta##. What do you calculate as ##\beta##, how did you get it? Please elaborate on what you are doing to get these numbers. Can you please share the plot? I think the variation you are seeing is noise, not the variation of ##\beta## as a function of ##v_{avg}##.
B= (Cd)(Area)(rho)(0.5)
Beta is all the constants. From here i just plug in what i have and get the Cd. Bellow is the plot of beta.

1677699326674.png
 
  • #101
LT72884 said:
B= (Cd)(Area)(rho)(0.5)
Beta is all the constants. From here i just plug in what i have and get the Cd. Bellow is the plot of beta.

View attachment 323057
Yeah, thats noise. Just do scatter plot, no line.
 
  • #102
erobz said:
Yeah, thats noise. Just do scatter plot, no line.
that is a scatter plot. Just connected with a line is all. if i remove the line, its the same mess haha

1677700711721.png
 
  • #103
LT72884 said:
that is a scatter plot. Just connected with a line is all. if i remove the line, its the same mess haha

View attachment 323058
How about some axis and scale?
 
  • #104
erobz said:
How about some axis and scale?
y axis is values where beta falls, x axis is the cell number. I have cells 2-39 selected
1677701533230.png
 
  • #105
even plotted against velocity as the x axis or even as a data set, its still looks scattered
 
  • #106
LT72884 said:
even plotted against velocity as the x axis or even as a data set, its still looks scattered
You are supposed to be plotting ##\beta## vs ##v_{avg}##? That is ##\beta## vs time; It's not really as useful. The purpose of this is to determine if ##\beta## depends on the velocity "##v_{avg}##"
 
  • #107
erobz said:
You are supposed to be plotting ##\beta## vs ##v_{avg}##? That is ##\beta## vs time; It's not really useful. The purpose of this is to determine if ##\beta## depends on the velocity "##v_{avg}##"
correct, and when i select that data, the velocity is a linear function with negative slope, and B is linear with 0 slope.
So somewhere, either excel is trying to be "smart" and adjust the data or i have selected the wrong data haha, which is possible
1677702651811.png
 
  • #108
LT72884 said:
correct, and when i select that data, the velocity is a linear function with negative slope, and B is linear with 0 slope.
So somewhere, either excel is trying to be "smart" and adjust the data or i have selected the wrong data haha, which is possible
View attachment 323060
You've plotted ##v_{avg}## vs time as a separate series. Delete the chart. Put in a blank one and right chart area - click "select data"

##v_{avg}## is the ##x## values
##\beta## is the ##y## values
 
  • #109
erobz said:
You've plotted ##v_{avg}## vs time as a separate series. Delete the chart. Put in a blank one and right chart area - click "select data"

##v_{avg}## is the ##x## values
##\beta## is the ##y## values
then what will the plotted data be? Im not sure i follow, but i will change the axis to match what you have said.
 
  • #110
i get the exact same thing
1677703296066.png
 
  • #111
LT72884 said:
then what will the plotted data be? Im not sure i follow, but i will change the axis to match what you have said.
It will be ##\beta## vs ##v_{avg}##
 
  • #112
erobz said:
It will be ##\beta## vs ##v_{avg}##
i get the exact same thing as post 104
1677703438400.png
 
  • #113
LT72884 said:
i get the exact same thing as post 104
I don't understand why there are so little a number of points?

This is what it should look like:

1677703454847.png
 
  • #114
erobz said:
I don't understand why there are so little a number of points?

This is what it should look like:

View attachment 323063
me niether. Let me close excel and refresh my RAM.. MAYBE some stupid glitch. I will be back shortly
 
  • #115
yup, something is not right. I selected all the average velocities as X and Beta as Y and this is my plot

1677703616590.png
 
  • #116
LT72884 said:
yup, something is not right. I selected all the average velocities as X and Beta as Y and this is my plot

View attachment 323064
Thats because of those data points that are near -30,000! Just chop the data off below 20 m/s.
 
  • #117
erobz said:
Thats because of those data points that are near -30,000! Just chop the data off below 20 m/s.
hmm, its better but not the same. i made sure no crazy values were in the mix either.
1677703970120.png
 
  • #118
LT72884 said:
hmm, its better but not the same. i made sure no crazy values were in the mix either.
View attachment 323065
Chop it off at 50 m/s
 
  • #119
i will keep chopping data back until it either changes or i find out of a wrong calculation

EDIT: i just saw your post stating the same thing as me.
 
  • #120
At 50m/s.
1677704341928.png

At 55m/s a drastic change
1677704401916.png
 

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