git: 6e361fe009e7 - main - cad/openvsp: update to 3.29.1

The branch main has been updated by fernape:

URL: https://cgit.FreeBSD.org/ports/commit/?id=6e361fe009e749dfd7566847232cd66540a1899d

commit 6e361fe009e749dfd7566847232cd66540a1899d
Author:     Fernando Apesteguía <fernape@FreeBSD.org>
AuthorDate: 2022-07-31 17:29:05 +0000
Commit:     Fernando Apesteguía <fernape@FreeBSD.org>
CommitDate: 2022-08-02 05:32:33 +0000

    cad/openvsp: update to 3.29.1
    
    3.29.1 reverts some changes to AngelScript related to Apple M1.
    The bulk of the changes are in 3.29.0.
    
    ChangeLog: http://openvsp.org/blogs/announcements/2022/07/26/openvsp-3-29-0-released
    
    Features
    
     * Optional quad meshing for CFDMesh and FEAMesh
     * Option to turn off high-order elements in FEAMesh
    
    VSPAERO Changes
    
     * Improved force (especially drag) calculations, and bug fixes there in.
     * Adjoint solver, stand alone now works for steady and usteady
     * Adjoint solver + solver = Optimizer with an API. (Steady and unsteady)
     * Initial API hooks for integration with OpenMDAO
     * Initial API hooks for tightly coupled structural solves
     * Complex step version should anyone care
     * Fix for thin/cusped trailing edges on panel meshes.
     * The degen geom and vspgeom files are both supported equally in terms of
       comp ids/surface
     * Sticking with DegenGeom for default VLM solves
     * VSPGEOM for Panel solves as default
     * Some of the output files have changed as folks were asking for more info in
       things like the span loading data, etc.
     * Cut planes added for solution visualization
     * Span loading for thick geometries
     * Preliminary supersonic panel support
     * Bugs. Some fixed, some added.
    
    Bug Fixes
    
     * Fix control surface addition for Wing Geoms
     * Silence echo of BEM file on read
     * Fix airfoil thickness scaling problem with blended wings
     * Fix VSPAERO Viewer movie creation on Windows (hopefully)
     * Fix int to float conversion overflow in InterpDistTable in CFDMesh
---
 cad/openvsp/Makefile  | 4 ++--
 cad/openvsp/distinfo  | 6 +++---
 cad/openvsp/pkg-plist | 5 ++++-
 3 files changed, 9 insertions(+), 6 deletions(-)

diff --git a/cad/openvsp/Makefile b/cad/openvsp/Makefile
index a4608faea729..629259a22f94 100644
--- a/cad/openvsp/Makefile
+++ b/cad/openvsp/Makefile
@@ -1,6 +1,6 @@
 PORTNAME=	openvsp
 DISTVERSIONPREFIX=	${GH_PROJECT}_
-DISTVERSION=	3.28.0
+DISTVERSION=	3.29.1
 CATEGORIES=	cad
 
 MAINTAINER=	fernape@FreeBSD.org
@@ -55,7 +55,7 @@ do-install:
 	@${MKDIR} ${STAGEDIR}${DATADIR}
 	${INSTALL_DATA} ${BUILD_WRKSRC}/${BUILD_PREFIX}/vspIcon.png ${STAGEDIR}${DATADIR}
 	${RM} ${STAGEDIR}${PREFIX}/vspIcon.png ${BUILD_WRKSRC}/${BUILD_PREFIX}/vspIcon.png
-.for f in vsp vspaero vspscript vspslicer vspviewer
+.for f in vsp vspaero vspaero_adjoint vspaero_complex vspaero_opt vsploads vspscript vspviewer
 	${INSTALL_PROGRAM} ${BUILD_WRKSRC}/${BUILD_PREFIX}/${f} ${STAGEDIR}${PREFIX}/bin
 	${RM} ${STAGEDIR}${PREFIX}/${f}
 .endfor
diff --git a/cad/openvsp/distinfo b/cad/openvsp/distinfo
index 797991b2e66d..0b6ddedee9ce 100644
--- a/cad/openvsp/distinfo
+++ b/cad/openvsp/distinfo
@@ -1,3 +1,3 @@
-TIMESTAMP = 1654061389
-SHA256 (OpenVSP-OpenVSP-OpenVSP_3.28.0_GH0.tar.gz) = e875f22460c03386685ff2ebf94e8fa72a9de30b784459e2a256a65d6a991dd7
-SIZE (OpenVSP-OpenVSP-OpenVSP_3.28.0_GH0.tar.gz) = 115459557
+TIMESTAMP = 1659288517
+SHA256 (OpenVSP-OpenVSP-OpenVSP_3.29.1_GH0.tar.gz) = 99351cbaeef0cc8a1f5706502a9986cb5b31a9f32176b76d417e98fc914cd275
+SIZE (OpenVSP-OpenVSP-OpenVSP_3.29.1_GH0.tar.gz) = 116340050
diff --git a/cad/openvsp/pkg-plist b/cad/openvsp/pkg-plist
index 4ad27287876a..a55df486437a 100644
--- a/cad/openvsp/pkg-plist
+++ b/cad/openvsp/pkg-plist
@@ -1,8 +1,11 @@
 README.md
 bin/vsp
 bin/vspaero
+bin/vspaero_adjoint
+bin/vspaero_complex
+bin/vspaero_opt
+bin/vsploads
 bin/vspscript
-bin/vspslicer
 bin/vspviewer
 %%DATADIR%%/23015.af
 %%DATADIR%%/AirfoilExport.vspscript