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diff --git a/api/flowunsteady-maneuver/index.html b/api/flowunsteady-maneuver/index.html
diff --git a/api/flowunsteady-monitor/index.html b/api/flowunsteady-monitor/index.html
diff --git a/api/flowunsteady-openvsp/index.html b/api/flowunsteady-openvsp/index.html
diff --git a/api/flowunsteady-postprocessing-fdom/index.html b/api/flowunsteady-postprocessing-fdom/index.html
diff --git a/api/flowunsteady-postprocessing-misc/index.html b/api/flowunsteady-postprocessing-misc/index.html
diff --git a/api/flowunsteady-postprocessing-noise/index.html b/api/flowunsteady-postprocessing-noise/index.html
diff --git a/api/flowunsteady-run/index.html b/api/flowunsteady-run/index.html
diff --git a/api/flowunsteady-simulation/index.html b/api/flowunsteady-simulation/index.html
diff --git a/api/flowunsteady-vehicle-asm/index.html b/api/flowunsteady-vehicle-asm/index.html
diff --git a/api/flowunsteady-vehicle-components/index.html b/api/flowunsteady-vehicle-components/index.html
diff --git a/api/flowunsteady-vehicle-types/index.html b/api/flowunsteady-vehicle-types/index.html
diff --git a/api/flowvpm-particle/index.html b/api/flowvpm-particle/index.html
diff --git a/api/flowvpm-relaxation/index.html b/api/flowvpm-relaxation/index.html
diff --git a/api/flowvpm-sfs/index.html b/api/flowvpm-sfs/index.html
diff --git a/api/flowvpm-time/index.html b/api/flowvpm-time/index.html
diff --git a/api/flowvpm-uj/index.html b/api/flowvpm-uj/index.html
diff --git a/api/flowvpm-utils/index.html b/api/flowvpm-utils/index.html
diff --git a/api/flowvpm-viscous/index.html b/api/flowvpm-viscous/index.html
diff --git a/examples/blownwing-acoustics/index.html b/examples/blownwing-acoustics/index.html
diff --git a/examples/blownwing-aero/index.html b/examples/blownwing-aero/index.html
diff --git a/examples/blownwing-asm/index.html b/examples/blownwing-asm/index.html
diff --git a/examples/heavingwing/index.html b/examples/heavingwing/index.html
diff --git a/examples/openvsp-aircraft/index.html b/examples/openvsp-aircraft/index.html
diff --git a/examples/propeller-J040/index.html b/examples/propeller-J040/index.html
diff --git a/examples/propeller-incidence/index.html b/examples/propeller-incidence/index.html
diff --git a/examples/propeller-jsweep/index.html b/examples/propeller-jsweep/index.html
diff --git a/examples/propeller-quasisteady/index.html b/examples/propeller-quasisteady/index.html
diff --git a/examples/prowim-aero/index.html b/examples/prowim-aero/index.html
diff --git a/examples/rotorhover-acoustics/index.html b/examples/rotorhover-acoustics/index.html
diff --git a/examples/rotorhover-aero/index.html b/examples/rotorhover-aero/index.html
diff --git a/examples/rotorhover-fdom/index.html b/examples/rotorhover-fdom/index.html
diff --git a/examples/rotorhover-quasisteady/index.html b/examples/rotorhover-quasisteady/index.html
diff --git a/examples/tetheredwing/index.html b/examples/tetheredwing/index.html
diff --git a/examples/vahana-maneuver/index.html b/examples/vahana-maneuver/index.html
diff --git a/examples/vahana-monitor/index.html b/examples/vahana-monitor/index.html
diff --git a/examples/vahana-run/index.html b/examples/vahana-run/index.html
diff --git a/examples/vahana-vehicle/index.html b/examples/vahana-vehicle/index.html
diff --git a/examples/wing-4p2aoa/index.html b/examples/wing-4p2aoa/index.html
diff --git a/examples/wing-aoasweep/index.html b/examples/wing-aoasweep/index.html
diff --git a/generate_examples_blownwing.jl b/generate_examples_blownwing.jl
@@ -8,7 +8,7 @@ remote_url = "https://edoalvar2.groups.et.byu.net/public/FLOWUnsteady/"
 open(joinpath(output_path, output_name*"-aero.md"), "w") do fout
 
     println(fout, """
-    # [Wing-on-Rotor Interactions](@id blownwingaero)
+    # [Wing-on-Prop Interactions](@id blownwingaero)
 
     ```@raw html
     <div style="position:relative;padding-top:50%;">
@@ -23,13 +23,13 @@ open(joinpath(output_path, output_name*"-aero.md"), "w") do fout
     In this example we show mount propellers on a swept wing.
     The wing is modeled using the actuator line model that represents the wing
     as a lifting line.
-    This wing model is accurate for capturing wing-on-rotor interactions.
+    This wing model is accurate for capturing wing-on-prop interactions.
     For instance, the rotor will experience an unsteady blade loading (and
     increased tonal noise) caused by the turning of the flow ahead of the wing
     leading edge.
     However, this simple wing model is not adecuate for capturing
-    rotor-on-wing interactions (see [the next two sections](@ref asm) to
-    accurately predict rotor-on-wing interactions).
+    prop-on-wing interactions (see [the next two sections](@ref asm) to
+    accurately predict prop-on-wing interactions).
 
     """)
 

diff --git a/generate_examples_prowim.jl b/generate_examples_prowim.jl
@@ -8,10 +8,10 @@ remote_url = "https://edoalvar2.groups.et.byu.net/public/FLOWUnsteady/"
 open(joinpath(output_path, output_name*"-aero.md"), "w") do fout
 
     println(fout, """
-    # [Rotor-on-Wing Interactions](@id prowimaero)
+    # [Prop-on-Wing Interactions](@id prowimaero)
 
     In this example we use the [actuator surface model](@ref asm) (ASM) to
-    accurately predict the effects of props blowing on a wing.
+    more accurately predict the effects of props blowing on a wing.
     This case simulates the PROWIM experiment in
     [Leo Veldhuis' dissertation](https://repository.tudelft.nl/islandora/object/uuid%3A8ffbde9c-b483-40de-90e0-97095202fbe3)
     (2005), and reproduces the validation study published in
@@ -37,7 +37,7 @@ open(joinpath(output_path, output_name*"-aero.md"), "w") do fout
     * ``^\\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 rotor-on-wing interactions, unless using `p_per_step=5`)
+    (Mid-low fidelity settings may be inadequate for capturing prop-on-wing interactions, unless using `p_per_step=5`)
 
 
     """)
@@ -95,9 +95,9 @@ open(joinpath(output_path, output_name*"-aero.md"), "w") do fout
     ```
 
     The favorable comparison with the experiment at \$\\alpha=0^\\circ\$ and
-    \$4^\\circ\$ confirms that ASM accurately predicts propeller-wing
+    \$4^\\circ\$ confirms that ASM accurately predicts prop-on-wing
     interactions up to a moderate angle of attack. At \$\\alpha=10^\\circ\$ we suspect
-    that the wing is mildly stalled, leading to a larger discrepancy (further
+    that the wing is mildly stalled in the experiment, leading to a larger discrepancy (further
     discussed in [Alvarez' Dissertation](https://scholarsarchive.byu.edu/etd/9589)[^1]
     and
     [Alvarez & Ning, 2023](https://arc.aiaa.org/doi/abs/10.2514/1.C037279)[^2]).

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diff --git a/installation/windows/index.html b/installation/windows/index.html
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diff --git a/theory/convergence/index.html b/theory/convergence/index.html
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