byuflowlab · EdoAlvarezR · Jan 22, 2024 · Jan 22, 2024 · Jan 22, 2024
diff --git a/README.md b/README.md
@@ -140,7 +140,7 @@ the different stages of design.
   > **Limitations:**
   > *Viscous drag and separation is only captured through airfoil lookup tables, without attempting to shed separation wakes*
   > *• Incompressible flow only (though wave drag can be captured through airfoil lookup tables)*
-  > *• CPU parallelization through OpenMP without support for distributed memory (no MPI, i.e., only single-node* runs)
+  > *• CPU parallelization through OpenMP without support for distributed memory (no MPI, i.e., only single-node runs)*
   >
   > *Coded in [the Julia language](https://www.infoworld.com/article/3284380/what-is-julia-a-fresh-approach-to-numerical-computing.html) for Linux, MacOS, and Windows WSL.*
 
@@ -161,12 +161,12 @@ More about the models inside FLOWUnsteady:
 See the following publications for an in-depth dive into the theory and validation:
 
 * E. J. Alvarez, J. Mehr, & A. Ning (2022), "FLOWUnsteady: An Interactional Aerodynamics Solver for Multirotor Aircraft and Wind Energy," *AIAA AVIATION Forum*. [**[VIDEO]**](https://youtu.be/SFW2X8Lbsdw) [**[PDF]**](https://scholarsarchive.byu.edu/facpub/5830/)
-* E. J. Alvarez & A. Ning (2022), "Reviving the Vortex Particle Method: A Stable Formulation for Meshless Large Eddy Simulation," *(accepted in AIAAJ)*. [**[PDF]**](https://arxiv.org/pdf/2206.03658.pdf)
 * E. J. Alvarez (2022), "Reformulated Vortex Particle Method and Meshless Large Eddy Simulation of Multirotor Aircraft.," *Doctoral Dissertation, Brigham Young University*. [**[VIDEO]**](https://www.nas.nasa.gov/pubs/ams/2022/08-09-22.html) [**[PDF]**](https://scholarsarchive.byu.edu/etd/9589/)
+* E. J. Alvarez & A. Ning (2023), "Stable Vortex Particle Method Formulation for Meshless Large-Eddy Simulation," *AIAA Journal*. [**[PDF]**](https://arc.aiaa.org/doi/epdf/10.2514/1.J063045)
 
 <p><br></p>
 
-### Examples
+### Examples and Tutorials
 
 **Propeller:** [[Tutorial](https://flow.byu.edu/FLOWUnsteady/examples/propeller-J040)] [[Validation](https://flow.byu.edu/FLOWUnsteady/theory/validation/#Propeller)]
 
@@ -180,11 +180,13 @@ See the following publications for an in-depth dive into the theory and validati
 
 **Blown Wing:** [[Tutorial](https://flow.byu.edu/FLOWUnsteady/examples/blownwing-aero)] [[Validation](https://flow.byu.edu/FLOWUnsteady/theory/validation/#Rotor-Wing-Interactions)]
 
-<p align="center">
-  <img src="http://edoalvar2.groups.et.byu.net/public/FLOWUnsteady/prowimhtp-wvol34-cropped00.jpg" alt="img" style="width:100%">
-</p>
+<p align="center"> <a href="https://www.youtube.com/watch?v=GfS3NoVrFfU&hd=1"> <img src="http://edoalvar2.groups.et.byu.net/public/FLOWUnsteady/youtube-rotorwing.png" alt="youtube.com/watch?v=GfS3NoVrFfU" style="width:70%"> </a> </p>
+
+
+**Ducted Fan:** [[Paper](https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=7676&context=facpub)]
+
+<p align="center"> <a href="https://www.youtube.com/watch?v=BQpar3A0X-w&hd=1"> <img src="http://edoalvar2.groups.et.byu.net/public/FLOWUnsteady/youtube-edf.png" alt="youtube.com/watch?v=BQpar3A0X-w" style="width:70%"> </a> </p>
 
-<p><br></p>
 
 **Airborne-Wind-Energy Aircraft:** [[Video](https://www.youtube.com/watch?v=iFM3B4_N2Ls)]
 
@@ -204,11 +206,12 @@ High-fidelity
 
 **Aeroacoustic Noise:** [[Tutorial](https://flow.byu.edu/FLOWUnsteady/examples/rotorhover-acoustics)] [[Validation](https://flow.byu.edu/FLOWUnsteady/theory/validation/#Rotor)]
 
+<p align="center"> <a href="https://www.youtube.com/watch?v=ntQjP6KbZDk&hd=1"> <img src="http://edoalvar2.groups.et.byu.net/public/FLOWUnsteady/youtube-vahananoise.png" alt="youtube.com/watch?v=ntQjP6KbZDk" style="width:70%"> </a> </p>
+
 <p align="center">
   <img src="http://edoalvar2.groups.et.byu.net/public/FLOWUnsteady/cfdnoise_ningdji_multi_005D_03_20.gif" alt="Vid" style="width:60%"/>
 </p>
 
-<p align="center"> <a href="https://www.youtube.com/watch?v=ntQjP6KbZDk&hd=1"> <img src="http://edoalvar2.groups.et.byu.net/public/FLOWUnsteady/youtube-vahananoise.png" alt="youtube.com/watch?v=ntQjP6KbZDk" style="width:70%"> </a> </p>
 
 
 
@@ -237,9 +240,9 @@ If you were to encounter any issues or have questions, please first read through
 [the documentation](https://flow.byu.edu/FLOWUnsteady/), [open/closed
 issues](https://github.com/byuflowlab/FLOWUnsteady/issues?q=is%3Aissue+is%3Aclosed),
 and [the discussion forum](https://github.com/byuflowlab/FLOWUnsteady/discussions?discussions_q=).
-If the issue still persists, please
-[open a new issue](https://github.com/byuflowlab/FLOWUnsteady/issues) and/or
-participate in [the discussion forum](https://github.com/byuflowlab/FLOWUnsteady/discussions?discussions_q=).
+If the issue still persists, please participate in
+[the discussion forum](https://github.com/byuflowlab/FLOWUnsteady/discussions?discussions_q=)
+and/or [open a new issue](https://github.com/byuflowlab/FLOWUnsteady/issues).
 
   * Developers/contributors : [Eduardo J. Alvarez](https://www.edoalvarez.com/) (main), [Cibin Joseph](https://github.com/cibinjoseph), [Judd Mehr](https://www.juddmehr.com/), [Ryan Anderson](https://flow.byu.edu/people/), [Eric Green](https://flow.byu.edu/people/)
   * Created           : Sep 2017

diff --git a/docs/src/examples/prowim-aero.md b/docs/src/examples/prowim-aero.md
@@ -1,5 +1,13 @@
 # [Prop-on-Wing Interactions](@id prowimaero)
 
+```@raw html
+  <img src="https://edoalvar2.groups.et.byu.net/public/FLOWUnsteady//veldhuis2004-expsetup01.png" alt="Pic here" style="width: 49%;"/>
+```
+
+```@raw html
+<br><br>
+```
+
 In this example we use the [actuator surface model](@ref asm) (ASM) to
 more accurately predict the effects of props blowing on a wing.
 This case simulates the PROWIM experiment in
@@ -10,25 +18,38 @@ This case simulates the PROWIM experiment in
 In this example you can vary the fidelity of the simulation setting the
 following parameters:
 
-| Parameter | Mid-low fidelity | Mid-high fidelity | High fidelity | Description |
-| :-------: | :--------------: | :---------------: | :-----------: | :---------- |
-| `n_wing` | `50` | `50` | `100` | Number of wing elements per semispan |
-| `n_rotor` | `12` | `20` | `50` | Number of blade elements per blade |
-| `nsteps_per_rev` | `36` | `36` | `72` | Time steps per revolution |
-| `p_per_step` | `2` | `5` | `5` | Particle sheds per time step |
-| `shed_starting` | `false` | `false` | `true` | Whether to shed starting vortex |
-| `shed_unsteady` | `false` | `false` | `true` | Whether to shed vorticity from unsteady loading |
-| `treat_wake` | `true` | `true` | `false` | Treat wake to avoid instabilities |
-| `vlm_vortexsheet_overlap` | `2.125/10` | `2.125/10` | `2.125` | Particle overlap in ASM vortex sheet |
-| `vpm_integration` | `vpm.euler` | RK3``^\star`` | RK3``^\star`` | VPM time integration scheme |
-| `vpm_SFS` | None``^\dag`` | Dynamic``^\ddag`` | Dynamic``^\ddag`` | VPM LES subfilter-scale model |
+| Parameter | Low fidelity | Mid-low fidelity | Mid-high fidelity | High fidelity | Description |
+| :-------: | :----------: | :--------------: | :---------------: | :-----------: | :---------- |
+| `n_wing` | `50` | `50` | `50` | `100` | Number of wing elements per semispan |
+| `n_rotor` | `12` | `12` | `20` | `50` | Number of blade elements per blade |
+| `nsteps_per_rev` | `36` | `36` | `36` | `72` | Time steps per revolution |
+| `p_per_step` | `2` | `5` | `5` | `5` | Particle sheds per time step |
+| `shed_starting` | `false` | `false` | `false` | `true` | Whether to shed starting vortex |
+| `shed_unsteady` | `false` | `false` | `false` | `true` | Whether to shed vorticity from unsteady loading |
+| `treat_wake` | `true` | `true` | `true` | `false` | Treat wake to avoid instabilities |
+| `vlm_vortexsheet_overlap` | `2.125/10` | `2.125/10` | `2.125/10` | `2.125` | Particle overlap in ASM vortex sheet |
+| `vpm_integration` | `vpm.euler` | `vpm.euler` | RK3``^\star`` | RK3``^\star`` | VPM time integration scheme |
+| `vpm_SFS` | None``^\dag`` | None``^\dag`` | Dynamic``^\ddag`` | Dynamic``^\ddag`` | VPM LES subfilter-scale model |
 
 * ``^\star``*RK3:* `vpm_integration = vpm.rungekutta3`
 * ``^\dag``*None:* `vpm_SFS = vpm.SFS_none`
 * ``^\ddag``*Dynamic:* `vpm_SFS = vpm.SFS_Cd_twolevel_nobackscatter`
 
-(Mid-low fidelity settings may be inadequate for capturing prop-on-wing interactions, unless using `p_per_step=5`)
+(Low fidelity settings may be inadequate for accurately capturing
+prop-on-wing interactions, but mid-low or higher should do well)
+
+As a reference, high-fidelity looks like this (except that the video shows
+a tip-mounted configuration with ailerons):
 
+```@raw html
+<div style="position:relative;padding-top:50%;">
+    <iframe style="position:absolute;left:0;top:0;height:80%;width:72%;"
+        src="https://www.youtube.com/embed/GfS3NoVrFfU?hd=1"
+        title="YouTube video player" frameborder="0"
+        allow="accelerometer; autoplay; clipboard-write; encrypted-media; gyroscope; picture-in-picture; web-share"
+        allowfullscreen></iframe>
+</div>
+```
 
 
 ```julia
@@ -626,7 +647,8 @@ end
 ```
 ```@raw html
 <span style="font-size: 0.9em; color:gray;"><i>
-    Mid-low fidelity run time: 13 minutes a Dell Precision 7760 laptop. <br>
+    Low fidelity run time: 13 minutes a Dell Precision 7760 laptop. <br>
+    Mid-low fidelity run time: 25 minutes a Dell Precision 7760 laptop. <br>
     Mid-high fidelity run time: 70 minutes a Dell Precision 7760 laptop. <br>
     High fidelity runtime: ~2 days on a 16-core AMD EPYC 7302 processor.
 </i></span>

diff --git a/docs/src/generate_examples_prowim.jl b/docs/src/generate_examples_prowim.jl
@@ -10,6 +10,14 @@ open(joinpath(output_path, output_name*"-aero.md"), "w") do fout
     println(fout, """
     # [Prop-on-Wing Interactions](@id prowimaero)
 
+    ```@raw html
+      <img src="$(remote_url)/veldhuis2004-expsetup01.png" alt="Pic here" style="width: 49%;"/>
+    ```
+
+    ```@raw html
+    <br><br>
+    ```
+
     In this example we use the [actuator surface model](@ref asm) (ASM) to
     more accurately predict the effects of props blowing on a wing.
     This case simulates the PROWIM experiment in
@@ -20,25 +28,38 @@ open(joinpath(output_path, output_name*"-aero.md"), "w") do fout
     In this example you can vary the fidelity of the simulation setting the
     following parameters:
 
-    | Parameter | Mid-low fidelity | Mid-high fidelity | High fidelity | Description |
-    | :-------: | :--------------: | :---------------: | :-----------: | :---------- |
-    | `n_wing` | `50` | `50` | `100` | Number of wing elements per semispan |
-    | `n_rotor` | `12` | `20` | `50` | Number of blade elements per blade |
-    | `nsteps_per_rev` | `36` | `36` | `72` | Time steps per revolution |
-    | `p_per_step` | `2` | `5` | `5` | Particle sheds per time step |
-    | `shed_starting` | `false` | `false` | `true` | Whether to shed starting vortex |
-    | `shed_unsteady` | `false` | `false` | `true` | Whether to shed vorticity from unsteady loading |
-    | `treat_wake` | `true` | `true` | `false` | Treat wake to avoid instabilities |
-    | `vlm_vortexsheet_overlap` | `2.125/10` | `2.125/10` | `2.125` | Particle overlap in ASM vortex sheet |
-    | `vpm_integration` | `vpm.euler` | RK3``^\\star`` | RK3``^\\star`` | VPM time integration scheme |
-    | `vpm_SFS` | None``^\\dag`` | Dynamic``^\\ddag`` | Dynamic``^\\ddag`` | VPM LES subfilter-scale model |
+    | Parameter | Low fidelity | Mid-low fidelity | Mid-high fidelity | High fidelity | Description |
+    | :-------: | :----------: | :--------------: | :---------------: | :-----------: | :---------- |
+    | `n_wing` | `50` | `50` | `50` | `100` | Number of wing elements per semispan |
+    | `n_rotor` | `12` | `12` | `20` | `50` | Number of blade elements per blade |
+    | `nsteps_per_rev` | `36` | `36` | `36` | `72` | Time steps per revolution |
+    | `p_per_step` | `2` | `5` | `5` | `5` | Particle sheds per time step |
+    | `shed_starting` | `false` | `false` | `false` | `true` | Whether to shed starting vortex |
+    | `shed_unsteady` | `false` | `false` | `false` | `true` | Whether to shed vorticity from unsteady loading |
+    | `treat_wake` | `true` | `true` | `true` | `false` | Treat wake to avoid instabilities |
+    | `vlm_vortexsheet_overlap` | `2.125/10` | `2.125/10` | `2.125/10` | `2.125` | Particle overlap in ASM vortex sheet |
+    | `vpm_integration` | `vpm.euler` | `vpm.euler` | RK3``^\\star`` | RK3``^\\star`` | VPM time integration scheme |
+    | `vpm_SFS` | None``^\\dag`` | None``^\\dag`` | Dynamic``^\\ddag`` | Dynamic``^\\ddag`` | VPM LES subfilter-scale model |
 
     * ``^\\star``*RK3:* `vpm_integration = vpm.rungekutta3`
     * ``^\\dag``*None:* `vpm_SFS = vpm.SFS_none`
     * ``^\\ddag``*Dynamic:* `vpm_SFS = vpm.SFS_Cd_twolevel_nobackscatter`
 
-    (Mid-low fidelity settings may be inadequate for capturing prop-on-wing interactions, unless using `p_per_step=5`)
+    (Low fidelity settings may be inadequate for accurately capturing
+    prop-on-wing interactions, but mid-low or higher should do well)
+
+    As a reference, high-fidelity looks like this (except that the video shows
+    a tip-mounted configuration with ailerons):
 
+    ```@raw html
+    <div style="position:relative;padding-top:50%;">
+        <iframe style="position:absolute;left:0;top:0;height:80%;width:72%;"
+            src="https://www.youtube.com/embed/GfS3NoVrFfU?hd=1"
+            title="YouTube video player" frameborder="0"
+            allow="accelerometer; autoplay; clipboard-write; encrypted-media; gyroscope; picture-in-picture; web-share"
+            allowfullscreen></iframe>
+    </div>
+    ```
 
     """)
 
@@ -73,7 +94,8 @@ open(joinpath(output_path, output_name*"-aero.md"), "w") do fout
     println(fout, """
     ```@raw html
     <span style="font-size: 0.9em; color:gray;"><i>
-        Mid-low fidelity run time: 13 minutes a Dell Precision 7760 laptop. <br>
+        Low fidelity run time: 13 minutes a Dell Precision 7760 laptop. <br>
+        Mid-low fidelity run time: 25 minutes a Dell Precision 7760 laptop. <br>
         Mid-high fidelity run time: 70 minutes a Dell Precision 7760 laptop. <br>
         High fidelity runtime: ~2 days on a 16-core AMD EPYC 7302 processor.
     </i></span>

diff --git a/docs/src/index.md b/docs/src/index.md
@@ -161,7 +161,7 @@ the different stages of design.
   > **Limitations:**
   > *Viscous drag and separation is only captured through airfoil lookup tables, without attempting to shed separation wakes*
   > *• Incompressible flow only (though wave drag can be captured through airfoil lookup tables)*
-  > *• CPU parallelization through OpenMP without support for distributed memory (no MPI, i.e., only single-node* runs)
+  > *• CPU parallelization through OpenMP without support for distributed memory (no MPI, i.e., only single-node runs)*
   >
   > *Coded in [the Julia language](https://www.infoworld.com/article/3284380/what-is-julia-a-fresh-approach-to-numerical-computing.html) for Linux, MacOS, and Windows WSL.*
 
@@ -186,14 +186,14 @@ More about the models inside FLOWUnsteady:
 See the following publications for an in-depth dive into the theory and validation:
 
 * E. J. Alvarez, J. Mehr, & A. Ning (2022), "FLOWUnsteady: An Interactional Aerodynamics Solver for Multirotor Aircraft and Wind Energy," *AIAA AVIATION Forum*. [**[VIDEO]**](https://youtu.be/SFW2X8Lbsdw) [**[PDF]**](https://scholarsarchive.byu.edu/facpub/5830/)
-* E. J. Alvarez & A. Ning (2022), "Reviving the Vortex Particle Method: A Stable Formulation for Meshless Large Eddy Simulation," *(accepted in AIAAJ)*. [**[PDF]**](https://arxiv.org/pdf/2206.03658.pdf)
 * E. J. Alvarez (2022), "Reformulated Vortex Particle Method and Meshless Large Eddy Simulation of Multirotor Aircraft.," *Doctoral Dissertation, Brigham Young University*. [**[VIDEO]**](https://www.nas.nasa.gov/pubs/ams/2022/08-09-22.html) [**[PDF]**](https://scholarsarchive.byu.edu/etd/9589/)
+* E. J. Alvarez & A. Ning (2023), "Stable Vortex Particle Method Formulation for Meshless Large-Eddy Simulation," *AIAA Journal*. [**[PDF]**](https://arc.aiaa.org/doi/epdf/10.2514/1.J063045)
 
 ```@raw html
 <p><br></p>
 ```
 
-### Examples
+### Examples and Tutorials
 
 **Propeller:** [[Tutorial](https://flow.byu.edu/FLOWUnsteady/examples/propeller-J040)] [[Validation](https://flow.byu.edu/FLOWUnsteady/theory/validation/#Propeller)]
 
@@ -226,15 +226,31 @@ See the following publications for an in-depth dive into the theory and validati
 **Blown Wing:** [[Tutorial](https://flow.byu.edu/FLOWUnsteady/examples/blownwing-aero)] [[Validation](https://flow.byu.edu/FLOWUnsteady/theory/validation/#Rotor-Wing-Interactions)]
 
 ```@raw html
-<p align="center">
-  <img src="http://edoalvar2.groups.et.byu.net/public/FLOWUnsteady/prowimhtp-wvol34-cropped00.jpg" alt="img" style="width:100%">
-</p>
+<div style="position:relative;padding-top:50%;">
+    <iframe style="position:absolute;left:0;top:0;height:80%;width:71.0%;"
+        src="https://www.youtube.com/embed/GfS3NoVrFfU?hd=1"
+        title="YouTube video player" frameborder="0"
+        allow="accelerometer; autoplay; clipboard-write; encrypted-media; gyroscope; picture-in-picture; web-share"
+        allowfullscreen></iframe>
+</div>
 ```
 
+
+
+**Ducted Fan:** [[Paper](https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=7676&context=facpub)]
+
 ```@raw html
-<p><br></p>
+<div style="position:relative;padding-top:50%;">
+    <iframe style="position:absolute;left:0;top:0;height:80%;width:71.0%;"
+        src="https://www.youtube.com/embed/BQpar3A0X-w?hd=1"
+        title="YouTube video player" frameborder="0"
+        allow="accelerometer; autoplay; clipboard-write; encrypted-media; gyroscope; picture-in-picture; web-share"
+        allowfullscreen></iframe>
+</div>
 ```
 
+
+
 **Airborne-Wind-Energy Aircraft:** [[Video](https://www.youtube.com/watch?v=iFM3B4_N2Ls)]
 
 ```@raw html
@@ -273,12 +289,6 @@ High-fidelity
 
 **Aeroacoustic Noise:** [[Tutorial](https://flow.byu.edu/FLOWUnsteady/examples/rotorhover-acoustics)] [[Validation](https://flow.byu.edu/FLOWUnsteady/theory/validation/#Rotor)]
 
-```@raw html
-<p align="center">
-  <img src="http://edoalvar2.groups.et.byu.net/public/FLOWUnsteady/cfdnoise_ningdji_multi_005D_03_20.gif" alt="Vid" style="width:60%"/>
-</p>
-```
-
 ```@raw html
 <div style="position:relative;padding-top:50%;">
     <iframe style="position:absolute;left:0;top:0;height:80%;width:71.0%;"
@@ -290,6 +300,13 @@ High-fidelity
 ```
 
 
+```@raw html
+<p align="center">
+  <img src="http://edoalvar2.groups.et.byu.net/public/FLOWUnsteady/cfdnoise_ningdji_multi_005D_03_20.gif" alt="Vid" style="width:60%"/>
+</p>
+```
+
+
 
 
 
@@ -319,9 +336,9 @@ If you were to encounter any issues or have questions, please first read through
 [the documentation](https://flow.byu.edu/FLOWUnsteady/), [open/closed
 issues](https://github.com/byuflowlab/FLOWUnsteady/issues?q=is%3Aissue+is%3Aclosed),
 and [the discussion forum](https://github.com/byuflowlab/FLOWUnsteady/discussions?discussions_q=).
-If the issue still persists, please
-[open a new issue](https://github.com/byuflowlab/FLOWUnsteady/issues) and/or
-participate in [the discussion forum](https://github.com/byuflowlab/FLOWUnsteady/discussions?discussions_q=).
+If the issue still persists, please participate in
+[the discussion forum](https://github.com/byuflowlab/FLOWUnsteady/discussions?discussions_q=)
+and/or [open a new issue](https://github.com/byuflowlab/FLOWUnsteady/issues).
 
   * Developers/contributors : [Eduardo J. Alvarez](https://www.edoalvarez.com/) (main), [Cibin Joseph](https://github.com/cibinjoseph), [Judd Mehr](https://www.juddmehr.com/), [Ryan Anderson](https://flow.byu.edu/people/), [Eric Green](https://flow.byu.edu/people/)
   * Created           : Sep 2017