Articles | Volume 11, issue 9
https://doi.org/10.5194/wes-11-3719-2026
© Author(s) 2026. This work is distributed under the Creative Commons Attribution 4.0 License.
SANDWake3D: a 3D parabolic RANS solver for atmospheric surface layers and turbine wakes
Download
- Final revised paper (published on 24 Sep 2026)
- Preprint (discussion started on 24 Nov 2025)
Interactive discussion
Status: closed
Comment types: AC – author | RC – referee | CC – community | EC – editor | CEC – chief editor
| : Report abuse
-
CC1: 'Comment on wes-2025-249', Blondel Frédéric, 27 Nov 2025
- AC1: 'Reply on CC1', Lawrence Cheung, 27 Nov 2025
-
RC1: 'Comment on wes-2025-249', Anonymous Referee #1, 09 Dec 2025
- AC2: 'Reply on RC1', Lawrence Cheung, 31 Jan 2026
-
RC2: 'Comment on wes-2025-249', Anonymous Referee #2, 29 Dec 2025
- AC3: 'Reply on RC2', Lawrence Cheung, 31 Jan 2026
Peer review completion
AR – Author's response | RR – Referee report | ED – Editor decision | EF – Editorial file upload
AR by Lawrence Cheung on behalf of the Authors (28 Feb 2026)
Author's response
Author's tracked changes
Manuscript
ED: Referee Nomination & Report Request started (03 Mar 2026) by Johan Meyers
RR by Anonymous Referee #1 (20 Mar 2026)
RR by Anonymous Referee #2 (01 Apr 2026)
ED: Reconsider after major revisions (19 Apr 2026) by Johan Meyers
AR by Lawrence Cheung on behalf of the Authors (31 May 2026)
Author's response
Author's tracked changes
Manuscript
ED: Referee Nomination & Report Request started (27 Jun 2026) by Johan Meyers
RR by Anonymous Referee #1 (07 Jul 2026)
RR by Anonymous Referee #2 (14 Jul 2026)
ED: Publish as is (14 Jul 2026) by Johan Meyers
ED: Publish as is (14 Jul 2026) by Sandrine Aubrun (Chief editor)
AR by Lawrence Cheung on behalf of the Authors (24 Jul 2026)
Manuscript
Dear Authors,
I have a question regarding your use of a forward-in-space numerical algorithm in your preprint. Since such algorithms only allow downstream information propagation, I assume there is no induction zone upstream of the actuator disk. In the absence of an induction zone, it is standard to inject the momentum deficit at the end of the near wake (as in Bradstock and Schlez, WES, 2020), or at the rotor plane if pressure is being solved for. Could you clarify whether this is the approach you have taken, or if I have misunderstood your method?
Additionally, I noticed that Equations (9) and (10)—and possibly others—are ill-posed when L equals zero, as this would result in division by zero.
Thank you for your time and clarification.