[Jsbsim-cvslogs] CVS: JSBSim/aircraft/pc7/Engines Propeller.xml, 1.1, 1.2

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

Update of /cvsroot/jsbsim/JSBSim/aircraft/pc7/Engines
In directory sfp-cvs-1.v30.ch3.sourceforge.com:/tmp/cvs-serv13458/Engines

Modified Files:
	Propeller.xml 
Log Message:
Small updates based on more accurate data and the latest AeromatiC++

Index: Propeller.xml
===================================================================
RCS file: /cvsroot/jsbsim/JSBSim/aircraft/pc7/Engines/Propeller.xml,v
retrieving revision 1.1
retrieving revision 1.2
diff -C2 -r1.1 -r1.2
*** Propeller.xml	6 Jun 2016 10:49:20 -0000	1.1
--- Propeller.xml	6 Jul 2016 07:48:14 -0000	1.2
***************
*** 23,34 ****
    <ixx> 6.01793 </ixx>
    <diameter unit="IN"> 95 </diameter>
!   <numblades> 4 </numblades>
!   <gearratio> 15.8224 </gearratio>
    <cp_factor> 1.00 </cp_factor>
!   <ct_factor> 1.00 </ct_factor>
!   <minpitch> 12 </minpitch>
    <maxpitch> 45 </maxpitch>
!   <minrpm> 2014.55 </minrpm>
!   <maxrpm> 2370.06 </maxrpm>
  
   <!-- thrust coefficient as a function of advance ratio and blade angle -->
--- 23,34 ----
    <ixx> 6.01793 </ixx>
    <diameter unit="IN"> 95 </diameter>
!   <numblades> 3 </numblades>
!   <gearratio> 18.75 </gearratio>
    <cp_factor> 1.00 </cp_factor>
!   <ct_factor> 1.10 </ct_factor>
!   <minpitch> -12 </minpitch>
    <maxpitch> 45 </maxpitch>
!   <minrpm> 1900 </minrpm>
!   <maxrpm> 2200 </maxrpm>
  
   <!-- thrust coefficient as a function of advance ratio and blade angle -->