diff --git a/aerodynamic_analysis/src/methods/liftingLineForTandem.cpp b/aerodynamic_analysis/src/methods/liftingLineForTandem.cpp
index 65378f039083fdd7bce40e80c4b05e097b5221a5..84b60e654b441ef9f7fa37606db838a7e72dd2c7 100644
--- a/aerodynamic_analysis/src/methods/liftingLineForTandem.cpp
+++ b/aerodynamic_analysis/src/methods/liftingLineForTandem.cpp
@@ -61,22 +61,21 @@ LiLiforTandemInitialization::LiLiforTandemInitialization()
}
liftingLineForTandem::liftingLineForTandem(const std::shared_ptr<RuntimeIO>& rtIO, const std::string& liftingLinePath,
- const LiLiforTandemInitialization& LiLiPolarInit)
+ const LiLiforTandemInitialization& LiLiInit)
:
- stepWidthCL(LiLiPolarInit.stepWidthCL),
- initialMachCruise(LiLiPolarInit.initialMachCruise),
- cruiseMachID(LiLiPolarInit.cruiseMachID),
+ stepWidthCL(LiLiInit.stepWidthCL),
+ initialMachCruise(LiLiInit.initialMachCruise),
+ cruiseMachID(LiLiInit.cruiseMachID),
designCL(0.2),
- bestCruiseCL(LiLiPolarInit.bestCruiseCL),
- CLModeAirfoilSelection(LiLiPolarInit.CLModeAirfoilSelection),
- indDragCtCorrForCalibration(LiLiPolarInit.indDragCtCorrForCalibration),
- factorDragCleanPolar(LiLiPolarInit.factorDragCleanPolar),
- liftingSurfaces(LiLiPolarInit.liftingSurfaces),
- flightConditions(LiLiPolarInit.flightConditions),
+ bestCruiseCL(LiLiInit.bestCruiseCL),
+ CLModeAirfoilSelection(LiLiInit.CLModeAirfoilSelection),
+ indDragCtCorrForCalibration(LiLiInit.indDragCtCorrForCalibration),
+ factorDragCleanPolar(LiLiInit.factorDragCleanPolar),
+ liftingSurfaces(LiLiInit.liftingSurfaces),
+ flightConditions(LiLiInit.flightConditions),
rtIO_(rtIO),
- delta_CM0(LiLiPolarInit.delta_CM0),
- delta_dCMdCL(LiLiPolarInit.delta_dCMdCL),
- currentIStabSetting(0.),
+ delta_CM0(LiLiInit.delta_CM0),
+ delta_dCMdCL(LiLiInit.delta_dCMdCL),
myLiftingLine(liftingLineInterface(liftingLinePath, rtIO->acxml.getName())),
myLiftingLine_compr(liftingLineInterface(liftingLinePath, rtIO->acxml.getName())) {
wingDesignPoint = new LiftDistributionPolarPoint();
@@ -85,6 +84,7 @@ liftingLineForTandem::liftingLineForTandem(const std::shared_ptr<RuntimeIO>& rtI
IOFilePath = rtIO_->acxml.getName();
config = rtIO_->aircraft_configuration_type();
airfoilPath = rtIO_->getAirfoilDataDir();
+ currentBackWingAngle = convertUnit(RADIAN, DEGREE, liftingSurfaces.back().sections.front().get_twist_angle());
}
void liftingLineForTandem::run(const Point& aCOG) {
@@ -627,7 +627,7 @@ void liftingLineForTandem::calculateCleanPolarForMach(const double& Mach, const
}
theCleanPolars.back().Points.back().AoA = (aLiftCoefficient - myLL_vec.at(Mach_id).theLLOutputPt->CLatAoA0) / dCLtodAoA_corr;
theCleanPolars.back().Points.back().CL = aLiftCoefficient;
- theCleanPolars.back().Points.back().iStabPolar = currentIStabSetting;
+ theCleanPolars.back().Points.back().iStabPolar = currentBackWingAngle;
// Calculate induced drag from LiftingLine
myRuntimeInfo->debug << " - Calculate drag ..." << endl;
this->calculateInducedDrag(Mach_id);
diff --git a/aerodynamic_analysis/src/methods/liftingLineForTandem.h b/aerodynamic_analysis/src/methods/liftingLineForTandem.h
index a3e97c848212eac37d812d6e16b92da021d8b2e5..460a7c6b249c7b3cc1f16a33f847e5f7533bf310 100644
--- a/aerodynamic_analysis/src/methods/liftingLineForTandem.h
+++ b/aerodynamic_analysis/src/methods/liftingLineForTandem.h
@@ -64,7 +64,7 @@ class liftingLineForTandem{
double bestCruiseCL;
double indDragCtCorrForCalibration;
double factorDragCleanPolar;
- double currentIStabSetting;
+ double currentBackWingAngle;
double delta_CM0;
double delta_dCMdCL;
// geometry
@@ -213,7 +213,7 @@ class liftingLineForTandem{
std::vector <double> yPositionsLL; /**< Vector of y positions used in Lifting Line calculations (subdivision of lifting surfaces) [m] */
/* Objects and functions for lifting line */
explicit liftingLineForTandem(const std::shared_ptr<RuntimeIO>& rtIO, const std::string& liftingLinePath,
- const LiLiforTandemInitialization& LiLiPolarInit);
+ const LiLiforTandemInitialization& LiLiInit);
virtual ~liftingLineForTandem() {}
// Polars
LiLiPolar aPolar();
diff --git a/aerodynamic_analysis/src/methods/tandemHighLiftAdaption.cpp b/aerodynamic_analysis/src/methods/tandemHighLiftAdaption.cpp
index c6ac78d101b7e1439da68a4572c7b2283d050974..e6f286584ed170dcf0c66915a3ff7a8c09b0f064 100644
--- a/aerodynamic_analysis/src/methods/tandemHighLiftAdaption.cpp
+++ b/aerodynamic_analysis/src/methods/tandemHighLiftAdaption.cpp
@@ -88,7 +88,7 @@ void tandemHighLiftAdaption::setHighLiftDevices() {
if (wingDevices.at(deviceID).name == "slat" ||
wingDevices.at(deviceID).name == "krueger" ||
wingDevices.at(deviceID).name == "droop_nose" ||
- wingDevices.at(deviceID).name == "morphing_droop_mose" ) {
+ wingDevices.at(deviceID).name == "morphing_droop_nose" ) {
leadingEdgeHighLiftDevices.push_back(wingDevices.at(deviceID));
}
}
@@ -133,7 +133,7 @@ void tandemHighLiftAdaption::processHighLiftDevices() {
double chordOutboard = getLocalChordLength(theFrontWing, trailingEdgeHighLiftDevices.at(deviceID).outerSpan_abs)
* fabs(trailingEdgeHighLiftDevices.at(deviceID).outerRelAftChordPosition - trailingEdgeHighLiftDevices.at(deviceID).outerRelFwdChordPosition);
// area is calculated for both devices, because symmetry
- trailingEdgeHighLiftDevices.at(deviceID).coveredA = leadingEdgeHighLiftDevices.at(deviceID).span * (chordInboard + chordOutboard);
+ trailingEdgeHighLiftDevices.at(deviceID).coveredA = trailingEdgeHighLiftDevices.at(deviceID).span * (chordInboard + chordOutboard);
}
}
@@ -218,7 +218,7 @@ void tandemHighLiftAdaption::setDeltaCLMaxDevices() {
}
}
-Polar tandemHighLiftAdaption::calculateHighLiftPolar(std::string config, const double CoG_X_position, const double currentIStabAngle) {
+Polar tandemHighLiftAdaption::calculateHighLiftPolar(std::string config, const double CoG_X_position, const double currentIBackWingAngle) {
this->theHighliftAdaption = this->setRaymerHighLiftAdaptionValues();
Polar aHighLiftPolar;
aHighLiftPolar.extrapolationMargin = theCleanPolar.extrapolationMargin;
@@ -360,7 +360,7 @@ Polar tandemHighLiftAdaption::calculateHighLiftPolar(std::string config, const d
}
aHighLiftPolar.PolarPoints.back().CM = (dCMtodCL_inc * aHighLiftPolar.PolarPoints.back().CL) + CMatCL0_inc
+ 0.5 * (factorLE + factorTE) * deltaHighLift;
- aHighLiftPolar.PolarPoints.back().iStabPolar = currentIStabAngle;
+ aHighLiftPolar.PolarPoints.back().iStabPolar = currentIBackWingAngle;
}
return aHighLiftPolar;
}
diff --git a/aerodynamic_analysis/src/methods/tandemHighLiftAdaption.h b/aerodynamic_analysis/src/methods/tandemHighLiftAdaption.h
index d7cd818ec90cbb5e39dac0e33b235e251c3958dc..132a209a2bfdce8c4370982f1fe76ebe86626909 100644
--- a/aerodynamic_analysis/src/methods/tandemHighLiftAdaption.h
+++ b/aerodynamic_analysis/src/methods/tandemHighLiftAdaption.h
@@ -92,7 +92,7 @@ class tandemHighLiftAdaption{
void processHighLiftDevices();
void setDeltaCLMaxDevices();
auto setRaymerHighLiftAdaptionValues() -> std::unordered_map<std::string, highLiftAdaption>;
- Polar calculateHighLiftPolar(std::string config, const double CoG_X_position, const double currentIStabAngle);
+ Polar calculateHighLiftPolar(std::string config, const double CoG_X_position, const double currentIBackWingAngle);
double getDeltaCMHighLift(const double CoG_X_Position, double Clift, double Mach, double CLmaxClean, double CLmaxHighLift);
double getAlphaAtCL(Polar aPolar, double aCL);
double getCLMax(Polar aPolar);
diff --git a/aerodynamic_analysis/src/tandem/tandemCalculatePolarConfig.cpp b/aerodynamic_analysis/src/tandem/tandemCalculatePolarConfig.cpp
index 3c4223d08e4d2468ffa54a6f941497f8575739e2..9fadb7c15087379110de389555ba80370cf7e992 100644
--- a/aerodynamic_analysis/src/tandem/tandemCalculatePolarConfig.cpp
+++ b/aerodynamic_analysis/src/tandem/tandemCalculatePolarConfig.cpp
@@ -178,7 +178,7 @@ void tandemCalculatePolarConfig::initializeTrimSettings() {
//backWingAngles = {90, 90, 90}; //TODO kayra:sadece fuselage ici kisma twist koyuyordu kodu degistirdim
neutralBackWingAngleID = 1;
} else if (backWingAngleGridMode.value() == "mode_1") {
- backWingAngles = {-6.0, -4.0, -2.0, 0.0, 0.2, 0.4, 0.6};
+ backWingAngles = {-6.0, -4.0, -2.0, 0.0, 2.0, 4.0, 6.0};
neutralBackWingAngleID = 3;
} else if (backWingAngleGridMode.value() == "mode_2") {
myRuntimeInfo->out << "read out custom angles not implemented yet, tschüss!" << endl;
diff --git a/aerodynamic_analysis/src/tandem/tandemDefaultStrategy.cpp b/aerodynamic_analysis/src/tandem/tandemDefaultStrategy.cpp
index 7707e3942336505cec7c6e8a6b4898219061c928..2b5f06bcf9db47bfe4bca7b278fa41d65086fd66 100644
--- a/aerodynamic_analysis/src/tandem/tandemDefaultStrategy.cpp
+++ b/aerodynamic_analysis/src/tandem/tandemDefaultStrategy.cpp
@@ -171,7 +171,7 @@ void tandemDefaultStrategy::createAircraftGeometry(const double backWingAngle) {
CGAL::IO::write_STL("tandemWing_mesh.stl", fuselage_mesh); //TODO kayra: cok yanlis suan:update geldi mi?
}
-void tandemDefaultStrategy::runAeroCalculations(const Point CoGPosition, const double currentIStabAngle) {
+void tandemDefaultStrategy::runAeroCalculations(const Point CoGPosition, const double currentIBackWingAngle) {
// lifting line for tandem
LiLiforTandemInitialization myLiLiInit;
this->initializeLiLiforTandem(&myLiLiInit);
@@ -195,7 +195,7 @@ void tandemDefaultStrategy::runAeroCalculations(const Point CoGPosition, const d
this->copyWingDevicesAndStabilizer(myTandemHLAdaption);
this->copyCleanPolarForHLCalculation(myTandemHLAdaption, myLiftingLineForTandem);
myTandemHLAdaption->runHighLiftAdaption();
- this->calculateHighLiftPolars(myTandemHLAdaption, CoGPosition.xCoordinate, currentIStabAngle);
+ this->calculateHighLiftPolars(myTandemHLAdaption, CoGPosition.xCoordinate, currentIBackWingAngle);
}
void tandemDefaultStrategy::initializeLiLiforTandem(LiLiforTandemInitialization *myLiLiInit) {
@@ -442,10 +442,10 @@ void tandemDefaultStrategy::copyCleanPolarForHLCalculation(tandemHighLiftAdaptio
myTandemHLAdaption->CMatAoA0 = myLiftingLineForTandem->theAnalyticalPolarData.CMatAoA0.at(0);
}
-void tandemDefaultStrategy::calculateHighLiftPolars(tandemHighLiftAdaption *myTandemHLAdaption, const double CoG_X_Position, const double currentIStabAngle) {
+void tandemDefaultStrategy::calculateHighLiftPolars(tandemHighLiftAdaption *myTandemHLAdaption, const double CoG_X_Position, const double currentIBackWingAngle) {
for (size_t configID(0); configID < HLconfigs.size(); ++configID) {
myRuntimeInfo->out << "Calculate high lift polar for " << HLconfigs.at(configID) << endl;
- Polar aPolar = myTandemHLAdaption->calculateHighLiftPolar(HLconfigs.at(configID), CoG_X_Position, currentIStabAngle);
+ Polar aPolar = myTandemHLAdaption->calculateHighLiftPolar(HLconfigs.at(configID), CoG_X_Position, currentIBackWingAngle);
currentPolarSet.highLiftPolars[HLconfigs.at(configID)] = tandemDefaultPolar();
// copy polar data
currentPolarSet.highLiftPolars.at(HLconfigs.at(configID)).Config = HLconfigs.at(configID);
@@ -465,8 +465,8 @@ void tandemDefaultStrategy::calculateHighLiftPolars(tandemHighLiftAdaption *myTa
}
}
-void tandemDefaultStrategy::copyPolarsToCGMap(const size_t CGID, const size_t stabID) {
- polarDataCGMap[CGID][stabID] = currentPolarSet;
+void tandemDefaultStrategy::copyPolarsToCGMap(const size_t CGID, const size_t backWingID) {
+ polarDataCGMap[CGID][backWingID] = currentPolarSet;
}
void tandemDefaultStrategy::clearDataForNextCalculationRun() {
@@ -481,26 +481,26 @@ void tandemDefaultStrategy::doTrimInterpolation() {
// copy polar data into the generalized interpolation container
for (size_t polarID(0); polarID < polarDataCGMap.at(CGID).at(0).cleanPolars.size(); ++polarID) {
myRuntimeInfo->out << "Interpolate trim for clean polars at " << config_->CGPositions.at(CGID) << " CoG at Ma " << config_->machNumbers.at(polarID) << "..." << endl;
- for (size_t stabID(0); stabID < config_->backWingAngles.size(); ++stabID) {
+ for (size_t backWingID(0); backWingID < config_->backWingAngles.size(); ++backWingID) {
vector<trimInterpolation::interpolationPoint> aStabPolar;
- for (size_t pointID(0); pointID < polarDataCGMap.at(CGID).at(stabID).cleanPolars.at(polarID).Points.size(); ++pointID) {
+ for (size_t pointID(0); pointID < polarDataCGMap.at(CGID).at(backWingID).cleanPolars.at(polarID).Points.size(); ++pointID) {
trimInterpolation::interpolationPoint anInterpolationPoint;
- anInterpolationPoint.CL = polarDataCGMap.at(CGID).at(stabID).cleanPolars.at(polarID).Points.at(pointID).CL;
- anInterpolationPoint.CM = polarDataCGMap.at(CGID).at(stabID).cleanPolars.at(polarID).Points.at(pointID).CM;
- anInterpolationPoint.values.push_back(polarDataCGMap.at(CGID).at(stabID).cleanPolars.at(polarID).Points.at(pointID).CD);
- anInterpolationPoint.values.push_back(polarDataCGMap.at(CGID).at(stabID).cleanPolars.at(polarID).Points.at(pointID).AoA);
- anInterpolationPoint.values.push_back(polarDataCGMap.at(CGID).at(stabID).cleanPolars.at(polarID).Points.at(pointID).iStabPolar);
- anInterpolationPoint.values.push_back(polarDataCGMap.at(CGID).at(stabID).cleanPolars.at(polarID).Points.at(pointID).CD_ind);
- anInterpolationPoint.values.push_back(polarDataCGMap.at(CGID).at(stabID).cleanPolars.at(polarID).Points.at(pointID).CD_visc);
- anInterpolationPoint.values.push_back(polarDataCGMap.at(CGID).at(stabID).cleanPolars.at(polarID).Points.at(pointID).CD_wave);
- anInterpolationPoint.values.push_back(polarDataCGMap.at(CGID).at(stabID).cleanPolars.at(polarID).PointsFrontWing.at(pointID).CD_wave);
- anInterpolationPoint.values.push_back(polarDataCGMap.at(CGID).at(stabID).cleanPolars.at(polarID).PointsBackWing.at(pointID).CD_ind);
- anInterpolationPoint.values.push_back(polarDataCGMap.at(CGID).at(stabID).cleanPolars.at(polarID).PointsBackWing.at(pointID).CD_wave);
+ anInterpolationPoint.CL = polarDataCGMap.at(CGID).at(backWingID).cleanPolars.at(polarID).Points.at(pointID).CL;
+ anInterpolationPoint.CM = polarDataCGMap.at(CGID).at(backWingID).cleanPolars.at(polarID).Points.at(pointID).CM;
+ anInterpolationPoint.values.push_back(polarDataCGMap.at(CGID).at(backWingID).cleanPolars.at(polarID).Points.at(pointID).CD);
+ anInterpolationPoint.values.push_back(polarDataCGMap.at(CGID).at(backWingID).cleanPolars.at(polarID).Points.at(pointID).AoA);
+ anInterpolationPoint.values.push_back(polarDataCGMap.at(CGID).at(backWingID).cleanPolars.at(polarID).Points.at(pointID).iStabPolar);
+ anInterpolationPoint.values.push_back(polarDataCGMap.at(CGID).at(backWingID).cleanPolars.at(polarID).Points.at(pointID).CD_ind);
+ anInterpolationPoint.values.push_back(polarDataCGMap.at(CGID).at(backWingID).cleanPolars.at(polarID).Points.at(pointID).CD_visc);
+ anInterpolationPoint.values.push_back(polarDataCGMap.at(CGID).at(backWingID).cleanPolars.at(polarID).Points.at(pointID).CD_wave);
+ anInterpolationPoint.values.push_back(polarDataCGMap.at(CGID).at(backWingID).cleanPolars.at(polarID).PointsFrontWing.at(pointID).CD_wave);
+ anInterpolationPoint.values.push_back(polarDataCGMap.at(CGID).at(backWingID).cleanPolars.at(polarID).PointsBackWing.at(pointID).CD_ind);
+ anInterpolationPoint.values.push_back(polarDataCGMap.at(CGID).at(backWingID).cleanPolars.at(polarID).PointsBackWing.at(pointID).CD_wave);
// interpolate additional values for cruise mach polar
- if (accuracyCheck(data_->initialCruiseMachNumber, polarDataCGMap.at(CGID).at(stabID).cleanPolars.at(polarID).MachNumber, ACCURACY_HIGH)) {
- anInterpolationPoint.vectorValues.push_back(polarDataCGMap.at(CGID).at(stabID).cleanPolars.at(polarID).PointsFrontWing.at(pointID).Cl_distr);
- anInterpolationPoint.vectorValues.push_back(polarDataCGMap.at(CGID).at(stabID).cleanPolars.at(polarID).PointsFrontWing.at(pointID).Lift_distr);
- anInterpolationPoint.vectorValues.push_back(polarDataCGMap.at(CGID).at(stabID).cleanPolars.at(polarID).PointsFrontWing.at(pointID).yStations);
+ if (accuracyCheck(data_->initialCruiseMachNumber, polarDataCGMap.at(CGID).at(backWingID).cleanPolars.at(polarID).MachNumber, ACCURACY_HIGH)) {
+ anInterpolationPoint.vectorValues.push_back(polarDataCGMap.at(CGID).at(backWingID).cleanPolars.at(polarID).PointsFrontWing.at(pointID).Cl_distr);
+ anInterpolationPoint.vectorValues.push_back(polarDataCGMap.at(CGID).at(backWingID).cleanPolars.at(polarID).PointsFrontWing.at(pointID).Lift_distr);
+ anInterpolationPoint.vectorValues.push_back(polarDataCGMap.at(CGID).at(backWingID).cleanPolars.at(polarID).PointsFrontWing.at(pointID).yStations);
}
aStabPolar.push_back(anInterpolationPoint);
}
@@ -862,12 +862,12 @@ void tandemDefaultStrategy::writePolarData() {
void tandemDefaultStrategy::writeViscDragData() {
ofstream plot;
for (size_t CGID(0); CGID < polarDataCGMap.size(); ++CGID) {
- for (size_t stabID(0); stabID < polarDataCGMap.at(CGID).size(); ++stabID) {
- for (size_t machID(0); machID < polarDataCGMap.at(CGID).at(stabID).cleanPolars.size(); ++machID) {
+ for (size_t backWingID(0); backWingID < polarDataCGMap.at(CGID).size(); ++backWingID) {
+ for (size_t machID(0); machID < polarDataCGMap.at(CGID).at(backWingID).cleanPolars.size(); ++machID) {
stringstream machNumber;
stringstream iStabStream;
- machNumber << setprecision(2) << fixed << polarDataCGMap.at(CGID).at(stabID).cleanPolars.at(machID).MachNumber;
- iStabStream << setprecision(2) << fixed << Rounding(config_->backWingAngles.at(stabID), 2);
+ machNumber << setprecision(2) << fixed << polarDataCGMap.at(CGID).at(backWingID).cleanPolars.at(machID).MachNumber;
+ iStabStream << setprecision(2) << fixed << Rounding(config_->backWingAngles.at(backWingID), 2);
std::string csvFile = "viscDrag_M" + replaceAll(machNumber.str(), ".", "") + "_"
+ CoGnames.at(CGID) + "_" + replaceAll(iStabStream.str(), ".", "") +"_plot.csv";
plot.open(csvFile.c_str());
@@ -876,20 +876,20 @@ void tandemDefaultStrategy::writeViscDragData() {
exit(1);
} else {
plot << "# " + csvFile << endl;
- plot << "# Reynolds Number" << polarDataCGMap.at(CGID).at(stabID).cleanPolars.at(machID).ReynoldsNumber << endl;
+ plot << "# Reynolds Number" << polarDataCGMap.at(CGID).at(backWingID).cleanPolars.at(machID).ReynoldsNumber << endl;
plot << "# Clean Polar" << endl;
- plot << "# Mach Number " << polarDataCGMap.at(CGID).at(stabID).cleanPolars.at(machID).MachNumber << endl;
+ plot << "# Mach Number " << polarDataCGMap.at(CGID).at(backWingID).cleanPolars.at(machID).MachNumber << endl;
plot << "AoA; C_L; C_D_visc; C_D_visc_Wing; C_D_visc_Stab; C_D_visc_Fin; C_D_visc_Fuselage; C_D_visc_Nacelles; C_D_visc_Misc;" << endl;
- for (size_t i(0); i < polarDataCGMap.at(CGID).at(stabID).cleanPolars.at(machID).Points.size(); ++i) {
- plot << setprecision(3) << fixed << polarDataCGMap.at(CGID).at(stabID).cleanPolars.at(machID).Points.at(i).AoA << ";";
- plot << setprecision(3) << fixed << polarDataCGMap.at(CGID).at(stabID).cleanPolars.at(machID).Points.at(i).CL << ";";
- plot << setprecision(6) << fixed << polarDataCGMap.at(CGID).at(stabID).cleanPolars.at(machID).Points.at(i).CD_visc << ";";
- plot << setprecision(6) << fixed << polarDataCGMap.at(CGID).at(stabID).cleanPolars.at(machID).PointsFrontWing.at(i).CD_visc << ";";
- plot << setprecision(6) << fixed << polarDataCGMap.at(CGID).at(stabID).cleanPolars.at(machID).PointsBackWing.at(i).CD_visc << ";";
- plot << setprecision(6) << fixed << polarDataCGMap.at(CGID).at(stabID).cleanPolars.at(machID).PointsFin.at(i).CD_visc << ";";
- plot << setprecision(6) << fixed << polarDataCGMap.at(CGID).at(stabID).cleanPolars.at(machID).PointsFuselage.at(i).CD_visc << ";";
- plot << setprecision(6) << fixed << polarDataCGMap.at(CGID).at(stabID).cleanPolars.at(machID).PointsNacelles.at(i).CD_visc << ";";
- plot << setprecision(6) << fixed << polarDataCGMap.at(CGID).at(stabID).cleanPolars.at(machID).PointsMisc.at(i).CD_visc << ";";
+ for (size_t i(0); i < polarDataCGMap.at(CGID).at(backWingID).cleanPolars.at(machID).Points.size(); ++i) {
+ plot << setprecision(3) << fixed << polarDataCGMap.at(CGID).at(backWingID).cleanPolars.at(machID).Points.at(i).AoA << ";";
+ plot << setprecision(3) << fixed << polarDataCGMap.at(CGID).at(backWingID).cleanPolars.at(machID).Points.at(i).CL << ";";
+ plot << setprecision(6) << fixed << polarDataCGMap.at(CGID).at(backWingID).cleanPolars.at(machID).Points.at(i).CD_visc << ";";
+ plot << setprecision(6) << fixed << polarDataCGMap.at(CGID).at(backWingID).cleanPolars.at(machID).PointsFrontWing.at(i).CD_visc << ";";
+ plot << setprecision(6) << fixed << polarDataCGMap.at(CGID).at(backWingID).cleanPolars.at(machID).PointsBackWing.at(i).CD_visc << ";";
+ plot << setprecision(6) << fixed << polarDataCGMap.at(CGID).at(backWingID).cleanPolars.at(machID).PointsFin.at(i).CD_visc << ";";
+ plot << setprecision(6) << fixed << polarDataCGMap.at(CGID).at(backWingID).cleanPolars.at(machID).PointsFuselage.at(i).CD_visc << ";";
+ plot << setprecision(6) << fixed << polarDataCGMap.at(CGID).at(backWingID).cleanPolars.at(machID).PointsNacelles.at(i).CD_visc << ";";
+ plot << setprecision(6) << fixed << polarDataCGMap.at(CGID).at(backWingID).cleanPolars.at(machID).PointsMisc.at(i).CD_visc << ";";
plot << endl;
}
}
diff --git a/aerodynamic_analysis/src/tandem/tandemDefaultStrategy.h b/aerodynamic_analysis/src/tandem/tandemDefaultStrategy.h
index 5038ee539bb2ce29e66852b63fcadbe90095b56c..19658cb09f7b73bba4a90f43fd5eaedb976ab713 100644
--- a/aerodynamic_analysis/src/tandem/tandemDefaultStrategy.h
+++ b/aerodynamic_analysis/src/tandem/tandemDefaultStrategy.h
@@ -95,7 +95,7 @@ class tandemDefaultStrategy {
/** \brief Function witch executes all aero calculation methods
* \param CoGPosition the 3D center of gravity coordinate as reference for the aero moments [m]
*/
- void runAeroCalculations(const Point CoGPosition, const double currentIStabAngle);
+ void runAeroCalculations(const Point CoGPosition, const double currentIBackWingAngle);
/** \brief Function to copy the polar set from liftingLinePolar to the strategyClass
* \param liftingLinePolar the lifting line for TAW method, which generated the clean polar set
*/
@@ -111,12 +111,12 @@ class tandemDefaultStrategy {
void sumUpDragComponents();
void copyWingDevicesAndStabilizer(tandemHighLiftAdaption *myTandemHLAdaption);
void copyCleanPolarForHLCalculation(tandemHighLiftAdaption *myTandemHLAdaption, liftingLineForTandem *myLiftingLineForTandem);
- void calculateHighLiftPolars(tandemHighLiftAdaption *myTandemHLAdaption, const double CoG_X_Position, const double currentIStabAngle);
+ void calculateHighLiftPolars(tandemHighLiftAdaption *myTandemHLAdaption, const double CoG_X_Position, const double currentIBackWingAngle);
/** \brief Copy the temporary current polar set to the permanent polarDataCGMap
* \param CGID index of the current center of gravity position
- * \param stabID index of the current stabilizer angle
+ * \param backWingID index of the current stabilizer angle
*/
- void copyPolarsToCGMap(const size_t CGID, const size_t stabID);
+ void copyPolarsToCGMap(const size_t CGID, const size_t backWingID);
/** \brief Function to delete temporary data befor next aero calculation run
*/
void clearDataForNextCalculationRun();