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Re: [Star-hp-l] STAR jet acoplanarity paper draft; request to form GPC
- From: Nihar Sahoo <nihar AT rcf.rhic.bnl.gov>
- To: "Ma, Rongrong" <marr AT bnl.gov>
- Cc: STAR HardProbes PWG <star-hp-l AT lists.bnl.gov>
- Subject: Re: [Star-hp-l] STAR jet acoplanarity paper draft; request to form GPC
- Date: Sat, 13 Jul 2024 23:05:22 +0530
Hello Rongrong,
I was traveling so I could not get time to work on your comments and reply.
After thinking on your comments, I realized my lower limit is not correct for R=0.2 case.
And I agree with you. I recalculated and included a section 3.14 and a Fig.29 in AN to show the lower limit of IAA calculation.
With this, I updated also Fig.3 and 6 in the paper draft.
Please find the version 3 paper draft: https://drupal.star.bnl.gov/STAR/system/files/AcoplanarityPaper_v3.pdf
And analysis note version-3 with Sec 3.14 and Fig.29:
https://drupal.star.bnl.gov/STAR/system/files/AcoplanarityAanalysisNote_V3.pdf
Please have a look.
For Fig. 28, I do not think the last bin matters since its yield isI will update this soon.
very very small. In any case, I am interested in your checks.
Best
Nihar
On 2024-06-24 23:38, Ma, Rongrong wrote:
Hello Nihar
Thanks for adding Sec. 3.14. However, it is not clear to me why the
limit (upper vs. lower) would change depending on whether the recoil
jet yield in pp is larger or smaller than that in AA. I_AA is defined
as Y_AA/Y_pp. As along as Y_pp is an upper limit, I think I_AA should
be the lower limit no matter if it is larger or smaller than 1. Maybe
I am missing something? Also, I feel the way you calculate the 95% CL
for I_AA probably needs some updates. Taking the ratio of 95% upper
limit for Y_pp to Y_AA+Err_AA would not give you I_AA with 95% CL. I
think one needs to use the central values of Y_pp and Y_AA to obtain
I_AA, and then calculate its 95% CL based on the uncertainties. If
this is not possible, you probably need some ToyMC to convolute the
probability distributions for Y_pp and Y_AA.
For Fig. 28, I do not think the last bin matters since its yield is
very very small. In any case, I am interested in your checks.
Thanks.
Best
Rongrong
On Jun 22, 2024, at 7:42 AM, Nihar Sahoo <nihar AT rcf.rhic.bnl.gov> wrote:
Hello Rongrong.
I have included the discussion of IAA upper and lower limit calculation in Section 3.14.
Please have a look at the updated AN: https://drupal.star.bnl.gov/STAR/system/files/AcoplanarityAanalysisNote_V2.pdf
I left Fig28 as it is because I calculated total yield by considering the last bin's mid point and by fitting the Y(dphi) for a consistency check. But I will check that calculation again during GPC discussion to update this fig, however I expect no big change).
Thank you
Nihar
On 2024-06-21 23:46, Ma, Rongrong wrote:
Hello Nihar
I do not think the last bin would cause the different I_AA shown in
Fig. 28, since its yield is very very small compared to other dphi
bins. The other bins closer to pi dominate recoil jet yields in pp and
AA, and thus I_AA.
Yes, indeed we discussed about the upper and lower limits before.
Sorry, I forgot about the details. From your response, do you mean
"For upper limit case, we take upper bound AuAu and lower bound of pp
in IAA calculation"? I could not find any details in the AN.
THanks.
Best
Rongrong
On Jun 21, 2024, at 1:42 PM, Nihar Sahoo <nihar AT rcf.rhic.bnl.gov> wrote:
Hello Rongrong,
Please find my replies inline.
On 2024-06-21 19:03, Ma, Rongrong wrote:
Hello NiharThank you for this crosscheck.
Thanks for the numerical values. If I sum up the recoil jet yields for
pp and AA, here is what I get.
1) pi0 trigger, R = 0.2, 10 < pT < 15 GeV/c
Y_AA = 0.030
Y_pp = 0.065 (the last bin with upper limit does not matter since its
yield is so much smaller than the other three dphi bins)
I_AA = Y_AA/Y_pp ~ 0.47
1) pi0 trigger, R = 0.2, 15 < pT < 20 GeV/c
Y_AA = 0.012
Y_pp = 0.063
I_AA = Y_AA/Y_pp ~ 0.19
These I_AA values are consistent with Fig. 3 in the paper, but not
Fig. 28 in AN where you demonstrate the consistency. Could you double
check the procedure for getting Fig. 28?
I have calculated considering that last bin's central value (but we only show upper limit in fig.2) just to have a consistency check. That could be the reason for Fig.28.As I am looking at this in more detail, another question arises. ForI remember, we had a discussion on this before if you recall.
pi0+jet measurements in p+p collisions, you have upper limits for the
dphi bin furthest to pi for both R = 0.2 and 0.5, which makes sense.
However, you have upper limits for I_AA for R = 0.5, and lower limits
for R = 0.2 jets. Why is this the case? How do you derive an upper
limit on I_AA given the upper limit on Y_pp?
But let me reiterate that to you here again.
For upper limit case, we take upper bound of pp and AuAu in IAA calculation.
similarly for lower bound, Lower limit of pp and AA.
Thank you
Nihar
P.S. Coming two weeks I will be traveling so I may be slow in replying.Thanks.
Best
Rongrong
On Jun 21, 2024, at 6:29 AM, Nihar Sahoo <nihar AT rcf.rhic.bnl.gov> wrote:
Hello Rongrong,
Please find the data points here.
Upper bound of last bin is mentioned there separately.
https://drupal.star.bnl.gov/STAR/blog/nihar/acoplanarity-pp-data
Thank you
Nihar
On 2024-06-21 01:09, Ma, Rongrong wrote:
Hello Nihar
Thanks for the numbers. Could you also send out the recoil jet yields
in pp and AA collisions for the four dphi bins between 2.2 and 3.14,
as shown in Fig. 2 of the paper? Could you do the same for 10-15 GeV/c
as well? Thanks.
Best
Rongrong
On Jun 20, 2024, at 2:59 PM, Nihar Sahoo <nihar AT rcf.rhic.bnl.gov> wrote:
Hello Rongrong,
As you mentioned this is a bit tricky to get exactly the same yield for two cases due to dphi weights and also unequal total dphi sum from Fig.2.
But I tried to estimate the yield for one case (15-20 GeV/c and R=0.2) and calculate IAA.
Here is the value 3.14 to 2.2 rad.
0.0033 (AA) /0.0109(pp) = 0.302 (IAA from Dphi) that is close to IAA(pT) ~0.3.
I have not considered uncertainty calculation.
Best
Nihar
On 2024-06-20 02:38, Ma, Rongrong wrote:
Hello Nihar
Thanks for updating Fig. 3 in the paper.
As you mentioned, different dPhi bins contribute differently to the
integrated recoil jet yields and I_AA for 2.35 < dphi < 3.14. However,
according to Fig. 2 of the paper, recoil jet yield drops exponentially
with decreasing dphi, so the new bins with upper limits that you just
added are furthest to dphi = 3.14, and thus contribute the least. It
is not clear to me how they can pull the integrated I_AA so
significantly. If possible, I suggest to directly compare recoil jet
yields for the two cases (vs. pt or vs. dphi). This can avoid the
complicated weighted average of I_AA.
Best
Rongrong
On Jun 19, 2024, at 12:07 PM, Nihar Sahoo <nihar AT rcf.rhic.bnl.gov> wrote:
Hello Rongrong,
Thank you for pointing this.
A updated upper bound for R=0.2 of 15-20 GeV/c pi0+jet case is included in paper Fig.3. (It was missed in previous draft but now corrected)
This one I checked it before.
For pi0+jet 15-20 GeV/c R=0.2 case:
As this is a differential measurement in Delta phi, each dphi contributes differently.
The last bin which is reported with upper bound is greater than I_AA=0.3 (see revised Fig.3), hence this bin contributes such that resultant integrated IAA(pTjet) value is around 0.3 (which is del_phi: 2.35 to 3.14 rad).
The same scenario is for 10-15 GeV/c for R=0.2; where the upper bound is lower than 0.3, and that contributes to Integrated IAA(pTjet) value.
The updated paper draft (same v2): https://drupal.star.bnl.gov/STAR/system/files/AcoplanarityPaper_v2.pdf
Best
Nihar
On 2024-06-19 03:35, Ma, Rongrong wrote:
Hello Nihar
Thanks a lot for addressing my comments. Those plots for consistency
check in AN are very useful. However, it is not clear how you extract
the I_AA values from dPhi differential measurement. Do you use the
same dPhi range and same pp reference as in I_AA(pT) analysis? In the
lower panel of Fig. 28, integrated I_AA(dphi) ~ 0.3 for pi0 triggers
and recoil R = 0.2 jets of 15 - 20 GeV/c. However, in Fig. 3, bottom
panel of the paper draft, I_AA values in all three dPhi bins are below
0.3. Why? The same question goes to pi0 trigger, recoil R = 0.2 jets
of 10-15 GeV/c. The integrated I_AA value is about 0.3 in AN, but all
three I_AA(dphi) values are above 0.4 in the paper draft.
Best
Rongrong
On Jun 18, 2024, at 4:25 AM, Nihar Sahoo via Star-hp-l <star-hp-l AT lists.bnl.gov> wrote:
Hello Rongrong, Yi , and Isaac,
Thank you for your constructive comments.
We have worked on your comments. Please find our responses at one place:
(Rongrong, Yi, and Isaac's comments are in order)
https://drupal.star.bnl.gov/STAR/system/files/PWGComments_Acoplanarity_June16.pdf
In this revised paper draft, Supplement material is included.
Revised paper draft (v2):https://drupal.star.bnl.gov/STAR/system/files/AcoplanarityPaper_v2.pdf
Revised AN v2: https://drupal.star.bnl.gov/STAR/system/files/AcoplanarityAanalysisNote_V2_0.pdf
We request HP-pwg converners to help us forming GPC.
Best
Nihar for PAs( Derek, Saskia, Peter)
On 2024-05-06 12:55, Yi Yang wrote:
Hi Nihar,_______________________________________________
Thanks a lot for the well-written draft and analysis note.
I agree with Rongrong's comments, so won't repeat here. I have some
minor ones for your consideration.
Paper draft:
- L36 - 38: the hyphens look a bit strange to me, it should look
like the one in L26. (similar for L314 and 315)
- L41: high energy --> high-energy
- L58: pT, jet > 30 GeV/c
- L59: R=0.3 --> R = 0.3
- L116: Gev --> GeV
- Eq.(1) and (2): it should be d^2 N_jet and d^2 sigma
- L156: sqrt(s_NN)=200 GeV --> sqrt(s_NN) = 200 GeV
- Figure 1: I would suggest to put the information in the right
panel to the left panel as well, just in case someone cut the left
panel only and there is no information on that.
- L229: What does "TBD" mean here? Will this affect the final
physics conclusion?
- L245: Fig.2 --> Figure 2
Question: (I probably asked it earlier) you show different behavior
for R = 0.2 and 0.5, does it make sense to try other R numbers to see
the actual R-dependence?
Analysis note:
- L172: Figure 23 --> Figure 9?
- Question: you are using PYTHIA-8 in the embedding/simulation, but
you used PYTHIA-6 for the comparison in the result. Why not use the
same version of PYTHIA?
- Don't you have the systematics from the unfolding iteration?
- Figure 23: It clearly shows the closure is not good between 2.5
and 3, and you are using log in the ratio. Any systematics associated
with it?
- L403, 404: there are "TBA"s, what does that mean?
- L435: The uncertainty on dPhi weights is "TBD"?
- Figure 26: do you have a similar plot for R = 0.2? What do the two
"light blue" lines mean here?
Cheers,
Yi
On Mon, Apr 8, 2024 at 10:16 AM Nihar Sahoo via Star-hp-l
<star-hp-l AT lists.bnl.gov> wrote:
Hello HP-pwg,https://drupal.star.bnl.gov/STAR/system/files/AcoplanarityPaper_v1.pdf
We have finalized STAR gamma+jet and pi0+jet acoplanarity paper
draft.
Paper draft, analysis Note, and paper webpage can be found below.
Please send your comment and feedback.
We request to form GPC.
Paper draft:
Analysis Note:https://drupal.star.bnl.gov/STAR/system/files/AcoplanarityAanalysisNote_V0_0.pdf
Paper webpage:https://drupal.star.bnl.gov/STAR/blog/nihar/Paper-webpage-Measurement-direct-photonjet-and-pi0jet-azimuthal-correlation-AuAu-and-pp-c
Thank you
PAs (Nihar, Derek, Saskia, and Peter)
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-
Re: [Star-hp-l] STAR jet acoplanarity paper draft; request to form GPC,
Nihar Sahoo, 07/13/2024
- Re: [Star-hp-l] STAR jet acoplanarity paper draft; request to form GPC, Ma, Rongrong, 07/15/2024
- <Possible follow-up(s)>
-
Re: [Star-hp-l] STAR jet acoplanarity paper draft; request to form GPC,
Nihar Sahoo, 07/13/2024
- Re: [Star-hp-l] STAR jet acoplanarity paper draft; request to form GPC, Ma, Rongrong, 07/15/2024
-
Re: [Star-hp-l] STAR jet acoplanarity paper draft; request to form GPC,
Yi Yang, 07/17/2024
- Re: [Star-hp-l] STAR jet acoplanarity paper draft; request to form GPC, Nihar Sahoo, 07/18/2024
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