Plot maps help file

update help files to include plot maps button.
nasa · Jan 14, 2016 · 5884209 · 5884209
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Showing 3 changed files with 27 additions and 14 deletions.
diff --git a/Trunk/TMATS_Library/TMATS_Support/Turbo_TMATS_Cmp.html b/Trunk/TMATS_Library/TMATS_Support/Turbo_TMATS_Cmp.html
@@ -79,6 +79,11 @@
     <tr><td>s_C_Wc_M</td><td>corrected flow scalar constant</td></tr>
     <tr><td>s_C_PR_M</td><td>pressure ratio scalar constant</td></tr>
     <tr><td>s_C_Eff_M</td><td>efficiency scalar constant</td></tr>
+    <tr><td>Plot Map</td><td>Plots the block defined map
+<br> - Include surge line - plots the surge line as defined in the Surge Margin tab on the map
+<br> - Scalars: none - plots maps as defined
+<br> - Scalars: user defined - plots maps with Wc, PR, and Eff scaled using the scalars defined in the C-map tab
+<br> - Scalars: iDesign - plots maps with Wc, PR, and Eff scaled using scalars calculated with iDesign and located within the file defined in the iDesign tab</td></tr>
     <tr><td>CBLDEN_M</td><td>Customer or flow based Bleed Enable [check - enabled]</td></tr>
     <tr><td>C_CBD_M</td><td>Customer or flow based Bleed Demand[pps](cbx1)</td></tr>
     <tr><td>C_CBFht_M</td><td>Customer or flow based Bleed Fractional enthalpy[frac](cbx1)</td></tr>

diff --git a/Trunk/TMATS_Library/TMATS_Support/Turbo_TMATS_Trb.html b/Trunk/TMATS_Library/TMATS_Support/Turbo_TMATS_Trb.html
@@ -65,6 +65,10 @@
     <tr><td>s_T_PR_M</td><td>Pressure Ratio Scalar Constant (T_PR)</td></tr>
     <tr><td>s_T_Wc_M</td><td>Flow Scalar Constant (T_Wc)</td></tr>
     <tr><td>s_T_Eff_M</td><td>Efficiency Scalar Constant (T_Eff)</td></tr>
+        <tr><td>Plot Map</td><td>Plots the block defined map
+            <br> - Scalars: none - plots maps as defined
+            <br> - Scalars: user defined - plots maps with Wc, PR, and Eff scaled using the scalars defined in the T-map tab
+    <br> - Scalars: iDesign - plots maps with Wc, PR, and Eff scaled using scalars calculated with iDesign and located within the file defined in the iDesign tab</td></tr>
     <tr><td>CFlwEn_M</td><td>Cooling Flow Enable [check - enabled]</td></tr>
     <tr><td>T_CoolFlwPos_M</td><td>Cooling Flow position [0 at inlet,  1 at exit](cx1)
             <br> With Cooling Flow Enabled, the turbine will expect cooling flow input 

diff --git a/Trunk/TMATS_Library/TMATS_Support/Turbo_TMATS_TrbNPSS.html b/Trunk/TMATS_Library/TMATS_Support/Turbo_TMATS_TrbNPSS.html
@@ -43,20 +43,20 @@
     <br>be driven to zero by an iterative solver</td></tr>
     <tr><td>TrqOut</td><td>turbine Torque Output (lbf*ft), positive value for a turbine.</td></tr>
     <tr><td>T_Data</td><td>Turbine internal calculation Data, 13x1 bus/vector including:
-    <br>- s_T_Nc - Corrected shaft speed map scalar value
-    <br>- s_T_Wc - Corrected mass flow map scalar value
-    <br>- s_T_PR - Pressure ratio map scalar value
-    <br>- s_T_Eff - Efficiency map scalar value
-    <br>- Wcin - Corrected mass flow input [pps]
-    <br>- Wcs1in - Corrected mass flow after station 1 (contains input bleed air) [pps]
-    <br>- Nc - Corrected shaft speed [rpm]
-    <br>- NcMap - Corrected shaft speed from the turbine map
-    <br>- WcMap - Corrected mass flow from the turbine map
-    <br>- PRMap - Pressure ratio from the turbine map
-    <br>- EffMap - Efficiency from the turbine map
-    <br>- Pwrout - output power [hp]
-    <br>- Test - Turbine interal calculation Data
-</td></tr>
+            <br>- s_T_Nc - Corrected shaft speed map scalar value
+            <br>- s_T_Wc - Corrected mass flow map scalar value
+            <br>- s_T_PR - Pressure ratio map scalar value
+            <br>- s_T_Eff - Efficiency map scalar value
+            <br>- Wcin - Corrected mass flow input [pps]
+            <br>- Wcs1in - Corrected mass flow after station 1 (contains input bleed air) [pps]
+            <br>- Nc - Corrected shaft speed [rpm]
+            <br>- NcMap - Corrected shaft speed from the turbine map
+            <br>- WcMap - Corrected mass flow from the turbine map
+            <br>- PRMap - Pressure ratio from the turbine map
+            <br>- EffMap - Efficiency from the turbine map
+            <br>- Pwrout - output power [hp]
+            <br>- Test - Turbine interal calculation Data
+    </td></tr>
 </table>
 <br>
 <font size="5" color="Blue">Turbine Mask Variables: </font>
@@ -69,6 +69,10 @@
     <tr><td>s_T_PR_M</td><td>Pressure Ratio Scalar Constant (T_PR)</td></tr>
     <tr><td>s_T_Wc_M</td><td>Flow Scalar Constant (T_Wc)</td></tr>
     <tr><td>s_T_Eff_M</td><td>Efficiency Scalar Constant (T_Eff)</td></tr>
+    <tr><td>Plot Map</td><td>Plots the block defined map
+            <br> - Scalars: none - plots maps as defined
+            <br> - Scalars: user defined - plots maps with Wc, PR, and Eff scaled using the scalars defined in the T-map tab
+    <br> - Scalars: iDesign - plots maps with Wc, PR, and Eff scaled using scalars calculated with iDesign and located within the file defined in the iDesign tab</td></tr>
     <tr><td>CFlwEn_M</td><td>Cooling Flow Enable [check - enabled]</td></tr>
     <tr><td>T_CoolFlwPos_M</td><td>Cooling Flow position [0 at inlet,  1 at exit](cx1)
             <br> With Cooling Flow Enabled, the turbine will expect cooling flow input