From 7100f67193f913609d9e530df416096df3eca002 Mon Sep 17 00:00:00 2001
From: acrovato <a.crovato@uliege.be>
Date: Sun, 14 May 2023 15:32:51 +0200
Subject: [PATCH] Remove references from README. Format.
---
README.md | 13 +------------
vii/src/DDriver.cpp | 4 +---
vii/src/DDriver.h | 2 +-
3 files changed, 3 insertions(+), 16 deletions(-)
diff --git a/README.md b/README.md
index 33f2de7..d1b7919 100644
--- a/README.md
+++ b/README.md
@@ -21,15 +21,4 @@ DART is currently capable of rapidly solving steady transonic flows on arbitrary
- [openMDAO](https://openmdao.org/)
## Documentation
-Detailed build and use instructions can be found in the [wiki](https://gitlab.uliege.be/am-dept/dartflo/wikis/home).
-
-## References
-Crovato Adrien, [Steady Transonic Aerodynamic and Aeroelastic Modeling for Preliminary Aircraft Design](http://hdl.handle.net/2268/251906), PhD thesis, University of Liège, 2020.
-
-Crovato Adrien, [DARTFlo - Discrete Adjoint for Rapid Transonic Flows](http://hdl.handle.net/2268/264284), Technical note, University of Liège, 2021.
-
-Crovato A., et al. [A discrete adjoint full potential formulation for fast aerostructural optimization in preliminary aircraft design](), Submitted to Aerospace Science and Technology, 2022.
-
-Crovato A., et al., [A Full Potential Static Aeroelastic Solver for Preliminary Aircraft Design](http://hdl.handle.net/2268/237955), 18th International Forum on Aeroelasticity and Structural Dynamics, IFASD 2019.
-
-Crovato A., et al., [Fast Full Potential Based Aerostructural Optimization Calculations for Preliminary Aircraft Design](http://hdl.handle.net/2268/292456), 19th International Forum on Aeroelasticity and Structural Dynamics, IFASD 2022.
+Detailed instructions for building and using the code, as well as references to theory manuals and scientific articles can be found in the [wiki](https://gitlab.uliege.be/am-dept/dartflo/wikis/home).
diff --git a/vii/src/DDriver.cpp b/vii/src/DDriver.cpp
index 35d8b3c..0828044 100644
--- a/vii/src/DDriver.cpp
+++ b/vii/src/DDriver.cpp
@@ -207,7 +207,7 @@ int Driver::run(unsigned int const couplIter)
pointExitCode = tSolver->integration(iPoint, sections[iSec][iRegion]);
// Force transition if required by the user
if (sections[iSec][iRegion]->xtrF != -1 && sections[iSec][iRegion]->mesh->getxoc(iPoint) >= sections[iSec][iRegion]->xtrF)
- sections[iSec][iRegion]->u[iPoint * sections[iSec][iRegion]->getnVar()+2] = 9.;
+ sections[iSec][iRegion]->u[iPoint * sections[iSec][iRegion]->getnVar() + 2] = 9.;
tms["1-Solver"].stop();
if (pointExitCode != 0)
@@ -765,8 +765,6 @@ std::vector<std::vector<double>> Driver::getSolution(size_t iSec)
Sln[17][nMarkersUp + iPoint] = sections[iSec][1]->mesh->gety(iPoint);
Sln[18][nMarkersUp + iPoint] = sections[iSec][1]->mesh->getz(iPoint);
Sln[19][nMarkersUp + iPoint] = sections[iSec][1]->blEdge->getVt(iPoint);
-
-
}
// Wake.
for (size_t iPoint = 0; iPoint < sections[iSec][2]->mesh->getnMarkers(); ++iPoint)
diff --git a/vii/src/DDriver.h b/vii/src/DDriver.h
index 3690a68..eddf310 100644
--- a/vii/src/DDriver.h
+++ b/vii/src/DDriver.h
@@ -38,7 +38,7 @@ protected:
public:
Driver(double _Re, double _Minf, double _CFL0, size_t nSections,
- double xtrF_top=-1., double xtrF_bot=-1., double _span = 0., unsigned int verbose = 1);
+ double xtrF_top = -1., double xtrF_bot = -1., double _span = 0., unsigned int verbose = 1);
~Driver();
int run(unsigned int const couplIter);
--
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