[Jsbsim-cvslogs] CVS: JSBSim/aircraft/paraglider paraglider.xml, 1.14, 1.15

[Erik H. <eh...@us...>]

Update of /cvsroot/jsbsim/JSBSim/aircraft/paraglider
In directory sfp-cvs-1.v30.ch3.sourceforge.com:/tmp/cvs-serv8566

Modified Files:
	paraglider.xml 
Log Message:
Model after a real paraglider model

Index: paraglider.xml
===================================================================
RCS file: /cvsroot/jsbsim/JSBSim/aircraft/paraglider/paraglider.xml,v
retrieving revision 1.14
retrieving revision 1.15
diff -C2 -r1.14 -r1.15
*** paraglider.xml	22 May 2016 12:19:30 -0000	1.14
--- paraglider.xml	23 May 2016 09:16:55 -0000	1.15
***************
*** 1,3 ****
! <?xml version="1.0"?>
  <?xml-stylesheet type="text/xsl" href="http://jsbsim.sourceforge.net/JSBSim.xsl"?>
  <fdm_config name="paraglider" version="2.0" release="BETA"
--- 1,3 ----
! <?xml version="1.0" encoding="UTF-8"?>
  <?xml-stylesheet type="text/xsl" href="http://jsbsim.sourceforge.net/JSBSim.xsl"?>
  <fdm_config name="paraglider" version="2.0" release="BETA"
***************
*** 16,25 ****
  
      http://www.cobaltcfd.com/pdfs/2016/AIAA-2016-1536.pdf
  -->
    </fileheader>
  
    <metrics>
!     <wingarea unit="FT2"> 300 </wingarea>
!     <wingspan unit="FT"> 32 </wingspan>
      <chord unit="FT"> 7 </chord>
      <htailarea unit="FT2"> 1 </htailarea>
--- 16,38 ----
  
      http://www.cobaltcfd.com/pdfs/2016/AIAA-2016-1536.pdf
+ 
+ 
+     http://www.ojovolador.com/eng/read/tests/discus/
+      Cells				44
+      Wing area (m²)			24	(258.33 ft²)
+      Wing area projected (m²)		20.5	(220.66 ft²)
+      Wing span (m)			11.2	( 36.75 ft)
+      Projected wing span (m)		 8.8	( 28.87 ft)
+      Aspect ratio			 5.2
+      Projected aspect ratio		 3.7
+      Glider weight (kg)			 4.9	( 10.8 lbs)
+      Max speed (km/h)			47 ±2	( 25.4 kts ±2)
+      Trim speed (km/h)			38 ±1	( 20.5 kts ±½)
  -->
    </fileheader>
  
    <metrics>
!     <wingarea unit="FT2"> 220 </wingarea>
!     <wingspan unit="FT"> 29 </wingspan>
      <chord unit="FT"> 7 </chord>
      <htailarea unit="FT2"> 1 </htailarea>
***************
*** 160,175 ****
    <aerodynamics>
  
!     <!--
!       Drag of a spehere: 	0.5
!        Re	CD(rough)	CD(clean)
!        10^2	1.2		1.2
!        10^3	0.5		0.5
!        10^4	0.5		0.5
!        10^5	0.2		0.5
!        50^5			0.1
!        10^6	0.4		0.35
!        10^7	0.5 		0.48
!     -->
!     <!-- pilot area (area of a circle with a diameter of 1.25 meter) -->
      <property type="float" value="13.2">metrics/Sp-sqft</property>
  
--- 173,177 ----
    <aerodynamics>
  
!     <!-- pilot area (area of a circle with a diameter of 4.1 foot) -->
      <property type="float" value="13.2">metrics/Sp-sqft</property>
  
***************
*** 364,367 ****
--- 366,370 ----
         <property>metrics/Sw-sqft</property>
         <property>metrics/bw-ft</property>
+        <value>2.5</value>
         <table>
          <independentVar lookup="row">aero/alpha-deg</independentVar>
***************
*** 523,540 ****
         <property>aero/ci2vel</property>
         <property>velocities/q-aero-rad_sec</property>
!        <value>-30</value>
! <!--
!        <table>
!         <independentVar>aero/alpha-deg</independentVar>
!         <tableData>
!            0.0  -1.9
!            2.0   0.5
!            4.0   0.0
!            6.0   2.9
!            8.0  -0.5
!           10.0   0.5
!         </tableData>
!        </table>
! -->
        </product>
       </function>
--- 526,543 ----
         <property>aero/ci2vel</property>
         <property>velocities/q-aero-rad_sec</property>
!        <sum>
!         <value>-20</value>
!         <table>
!          <independentVar>aero/alpha-deg</independentVar>
!          <tableData>
!             0.0  -1.9
!             2.0   0.5
!             4.0   0.0
!             6.0   2.9
!             8.0  -0.5
!            10.0   0.5
!          </tableData>
!         </table>
!        </sum>
        </product>
       </function>
***************
*** 548,551 ****
--- 551,555 ----
         <property>metrics/Sw-sqft</property>
         <property>metrics/bw-ft</property>
+        <value>2.5</value>
         <table>
          <independentVar lookup="row">aero/alpha-deg</independentVar>