updated documentation and setup script. added license

Author: andrewning

CHANGELOG.md

@@ -1,5 +1,22 @@
 # CCBlade Changelog
 
+## 1.0 (Sep 26, 2013)
+
+Andrew Ning <[email protected]>
+
+[NEW]:
+
+- analytic gradients!
+- presweep is added, but only from a blade element perspective---there are no sweep corrections.
+- added unit tests for gradients as compared to finite differencing
+
+[CHANGE]:
+
+- redefined the way precurvature is specified so that it was not implicitly coupled with rotor hub precone
+- no longer add the 0.0 loads at root and tip
+- simplified some of the outputs
+- removed direct dependence on coordinate system methods so that it could more easily stand-alone
+
 
 ## 0.3.0 (July 24, 2013)
 

LICENSE.txt

@@ -0,0 +1,13 @@
+Copyright 2012 NREL
+
+Licensed under the Apache License, Version 2.0 (the "License");
+you may not use this file except in compliance with the License.
+You may obtain a copy of the License at
+
+   http://www.apache.org/licenses/LICENSE-2.0
+
+Unless required by applicable law or agreed to in writing, software
+distributed under the License is distributed on an "AS IS" BASIS,
+WITHOUT WARRANTIES OR CONDITIONS OF ANY KIND, either express or implied.
+See the License for the specific language governing permissions and
+limitations under the License.

MANIFEST.in

@@ -0,0 +1,5 @@
+include README.md
+include CHANGELOG.md
+include LICENSE.txt
+graft docs/_build/html
+graft test

README.md

@@ -1,6 +1,6 @@
 # CCBlade
 
-A blade element momentum method for analyzing wind turbine aerodynamic performance that is robust (guaranteed convergence), fast (superlinear convergence rate), and smooth (continuously differentiable).  Analytic gradients are also (optionally) provided for the distributed loads, thrust, torque, and power with respect to most any design variable of interest.
+A blade element momentum method for analyzing wind turbine aerodynamic performance that is robust (guaranteed convergence), fast (superlinear convergence rate), and smooth (continuously differentiable).  Analytic gradients are also (optionally) provided for the distributed loads, thrust, torque, and power with respect to design variables of interest.
 
 Author: S. Andrew Ning
 

docs/UserGuide.pdf

@@ -22,8 +22,8 @@
 codeName = u'CCBlade'
 authorName = u'S. Andrew Ning'
 copyright = u'2013, NREL'
-version = '0.3'
-release = '0.3.0'
+version = '1.0'
+release = '1.0.0'
 
 # -- General configuration -----------------------------------------------------