Update README.md

README.md

@@ -20,12 +20,13 @@ The simulations were performed using the **"Fidelity Charles"** flow-solver, an
 * **Turbulence Modeling:** To capture complex, unsteady flow phenomena such as massive flow separation, a wall-modeled LES using the Dynamic Smagorinsky subgrid-scale model and an equilibrium wall model were employed.
 
 ## How to Cite This Dataset
-In order to cite the use of this dataset, please cite the corresponding preprint paper:
+In order to cite the use of this dataset, please cite the corresponding preprint paper (https://arxiv.org/abs/2605.19565):
 
 ```bibtex
 @article{ashton2026hiliftaeroml,
   title={{HiLiftAeroML: High-Fidelity Computational Fluid Dynamics Dataset for High-Lift Aircraft Aerodynamics}},
   year={2026},
+  journal = {arxiv.org}, url={https://arxiv.org/abs/2605.19565}, 
   author={Ashton, Neil and Clark, Adam and Heidt, Liam and Ivey, Christopher and Bose, Sanjeeb and Agrawal, Rahul and Goc, Konrad and Ranade, Rishi and Adams, Corey and Sharpe, Peter and Nidhan, Sheel and Akkurt, Semit and Leibovici, Daniel and Kossaifi, Jean}
 }
 ```