ZNP-K: Initial version.

andgi · Aug 17, 2011 · 7f2102f · 7f2102f
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diff --git a/AUTHORS b/AUTHORS
@@ -0,0 +1,43 @@
+US Navy ZNP-K / Goodyear K-Type airship flight model for JSBSim.
+
+    Copyright (C) 2010 - 2011  Anders Gidenstam  (anders(at)gidenstam.org)
+
+    This program is free software; you can redistribute it and/or modify
+    it under the terms of the GNU General Public License as published by
+    the Free Software Foundation; either version 2 of the License, or
+    (at your option) any later version.
+
+    This program is distributed in the hope that it will be useful,
+    but WITHOUT ANY WARRANTY; without even the implied warranty of
+    MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE.  See the
+    GNU General Public License for more details.
+
+    You should have received a copy of the GNU General Public License
+    along with this program; if not, write to the Free Software
+    Foundation, Inc., 59 Temple Place, Suite 330, Boston, MA  02111-1307  USA
+
+
+Anders Gidenstam  (anders(at)gidenstam.org)
+  - ZNP-K FlightGear configuration
+  - ZNP-K Flight Dynamics Model configuration
+  - ZNP-K 3d model
+
+The model borrows content from the following authors' contributions
+to FlightGear:
+
+Emmanuel BARANGER
+  - R1340 engines (scaled by 1.45). (From FlightGear/Aircraft/Sikorsky-S38)
+  - Propellers. (From FlightGear/Aircraft/B-25)
+
+Dependencies:
+
+Aircraft/Short_Empire   Instruments/SmithForeAftLevel/smith_fore_aft_level.*
+Aircraft/ZLT-NT         Systems/ground_handling.nas
+                        Systems/mp-network.nas
+                        Models/GroundCrew/scania-mast-truck.xml
+
+Potential use:
+Aircraft/p51d
+p51d/Models/p51d-jw-remote.*
+p51d/Models/p51d-jw-vsi.*
+p51d/Models/switch.ac
diff --git a/Engines/eng_PWR-1430-AN2.xml b/Engines/eng_PWR-1430-AN2.xml
@@ -0,0 +1,45 @@
+<?xml version="1.0"?>
+<!--
+  Pratt and Whitney R-1340-AN2 for JSBSim
+
+    Copyright (C) 2010  Anders Gidenstam  (anders(at)gidenstam.org)
+    This file is licensed under the GPL license version 2 or later.
+
+  <reference
+   refID="FAA:TC-5E-2"
+   author="FAA"
+   title="http://www.airweb.faa.gov/Regulatory_and_Guidance_Library/rgMakeModel.nsf/0/557844629a50a6388525676a006740c9/$FILE/ATTY2APL/5E-2.pdf"
+   date="?"/>
+
+-->
+<piston_engine name="R-1340-AN2">
+ <displacement unit="IN3"> 1344.0 </displacement>
+ <bore unit="IN">            5.75 </bore>
+ <stroke unit="IN">          5.75 </stroke>
+ <compression-ratio>         6.00 </compression-ratio>
+ <cylinders>                 9.00 </cylinders>
+ <cycles>                    4.00 </cycles>
+
+ <maxhp>                   600.0 </maxhp>
+ <!--bsfc>                      0.37 </bsfc-->
+ <!--volumetric-efficiency>     0.85 </volumetric-efficiency -->
+ <idlerpm>                 550.0 </idlerpm>
+ <maxrpm>                 2250.0 </maxrpm>
+
+ <numboostspeeds> 1.0 </numboostspeeds>
+ <boostoverride>  0 </boostoverride>
+
+ <ratedboost1 unit="INHG">     2.58 </ratedboost1>
+ <ratedpower1 unit="HP">     550.00 </ratedpower1>
+ <ratedrpm1>                2200.00 </ratedrpm1>
+ <ratedaltitude1 unit="FT"> 5000.00 </ratedaltitude1>
+
+ <takeoffboost unit="INHG">    6.08 </takeoffboost>
+
+ <sparkfaildrop>               0.10 </sparkfaildrop>
+
+ <minmp unit="INHG">           6.50 </minmp> <!-- Deprecated -->
+ <maxmp unit="INHG">          36.00 </maxmp>
+ <maxthrottle>                 1.00 </maxthrottle>
+ <minthrottle>                 0.10 </minthrottle>
+</piston_engine>
diff --git a/Engines/prop_HamiltonStd5415.xml b/Engines/prop_HamiltonStd5415.xml
@@ -0,0 +1,126 @@
+<?xml version="1.0"?>
+<!--
+  Hamilton Standard 5415 for Goodgear K-Type airship for JSBSim
+
+    Copyright (C) 2010 - 2011  Anders Gidenstam  (anders(at)gidenstam.org)
+    This file is licensed under the GPL license version 2 or later.
+
+-->
+<propeller name="Hamilton Standard 5415">
+
+ <documentation>
+  [GAC:1942:PM]:
+   Engine     R-1340-AN2  425 H.P. at 1775 RPM (engine or prop RPM?).
+   Propellers 3 blades 12' 0" diameter (K9- K-13)
+   Propellers 3 blades 12' 6" diameter (K-14 -)
+   Average performance:
+     Knots    RPM(prop/eng?)  Fuel lb/hr  
+       40      1050            102
+       50      1290            148
+       67.5    1740            400
+
+  [GAC:1942:DS]:
+   Propellers (K-14 and Future):
+     "3-bladed, 12'-6" dia., Hartzell Type aluminum alloy blades"
+ </documentation>
+
+ <documentation>
+   JavaProp:
+     Designed for 70 knots (maximum speed in level flight)
+     at 450 HP and 1800 (engine) RPM at coarse pitch.
+     Fine pitch is design pitch -? deg (a guess).
+
+     #blades 3
+     n          1200 RPM
+     D          3.81 m
+     Spinner D  0.200 m
+     Velocity   36.011111 m/s
+     Power      335564.94 W
+     Weight     ? lb
+
+   Airfoil
+     Clark Y, Re=500000
+     Clark Y, Re=500000
+     Clark Y, Re=500000
+     Flat plate, Re=500000
+ </documentation>
+
+ <ixx>307.36632</ixx>
+ <diameter unit="IN">150.0</diameter>
+ <numblades> 3 </numblades>
+ <gearratio> 1.5 </gearratio>
+ <minpitch>  12.0 </minpitch>
+ <maxpitch>  22.0 </maxpitch>
+ <!-- minrpm>  400.0 </minrpm -->
+ <!-- maxrpm> 1200.0 </maxrpm -->
+
+ <ct_factor> 1.00 </ct_factor>
+ <cp_factor> 1.20 </cp_factor> <!-- Tweak -->
+
+ <table name="C_THRUST" type="internal">
+  <tableData>
+             12.0      17.0      22.0
+   0.00000   0.07034   0.09028   0.10233
+   0.05000   0.02952   0.08471   0.10365
+   0.10000   0.01926   0.08063   0.10244
+   0.15000   0.04112   0.04202   0.10046
+   0.20000   0.03426   0.07015   0.04429
+   0.25000   0.02616   0.06334   0.09474
+   0.30000   0.01751   0.05502   0.09096
+   0.35000   0.00794   0.04600   0.08505
+   0.40000  -0.00207   0.03666   0.07744
+   0.45000  -0.01276   0.02690   0.06810
+   0.50000  -0.02365   0.01660   0.05862
+   0.55000  -0.03455   0.00579   0.04883
+   0.60000  -0.04544  -0.00550   0.03858
+   0.65000  -0.05634  -0.01723   0.02791
+   0.70000  -0.06723  -0.02896   0.01686
+   0.75000  -0.07813  -0.04069   0.00546
+   0.80000  -0.08902  -0.05242  -0.00637
+   0.85000  -0.09992  -0.06415  -0.01840
+   0.90000  -0.11081  -0.07588  -0.03043
+   0.95000  -0.12171  -0.08761  -0.04246
+   1.00000  -0.13260  -0.09934  -0.05449
+   1.05000  -0.14350  -0.11107  -0.06652
+   1.10000  -0.15439  -0.12280  -0.07855
+   1.15000  -0.16529  -0.13453  -0.09058
+   1.20000  -0.17618  -0.14626  -0.10261
+   1.25000  -0.18708  -0.15799  -0.11464
+   1.30000  -0.19797  -0.16972  -0.12667
+  </tableData>
+ </table>
+
+ <table name="C_POWER" type="internal">
+  <tableData>
+             12.0      17.0      22.0
+   0.00000   0.01793   0.03282   0.05236
+   0.05000   0.01203   0.03293   0.05288
+   0.10000   0.00987   0.03274   0.05241
+   0.15000   0.01580   0.01806   0.05240
+   0.20000   0.01452   0.03134   0.02102
+   0.25000   0.01273   0.02991   0.05196
+   0.30000   0.01044   0.02770   0.05156
+   0.35000   0.00746   0.02487   0.05044
+   0.40000   0.00387   0.02146   0.04813
+   0.45000  -0.00051   0.01745   0.04455
+   0.50000   0.01000   0.01277   0.04042
+   0.55000   0.01000   0.00732   0.03562
+   0.60000   0.01000   0.00102   0.03003
+   0.65000   0.01000   0.01000   0.02362
+   0.70000   0.01000   0.01000   0.01639
+   0.75000   0.01000   0.01000   0.00837
+   0.80000   0.01000   0.01000  -0.00060
+   0.85000   0.01000   0.01000   0.01000
+   0.90000   0.01000   0.01000   0.01000
+   0.95000   0.01000   0.01000   0.01000
+   1.00000   0.01000   0.01000   0.01000
+   1.05000   0.01000   0.01000   0.01000
+   1.10000   0.01000   0.01000   0.01000
+   1.15000   0.01000   0.01000   0.01000
+   1.20000   0.01000   0.01000   0.01000
+   1.25000   0.01000   0.01000   0.01000
+   1.30000   0.01000   0.01000   0.01000
+  </tableData>
+ </table>
+
+</propeller>