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Merge pull request #44 from giovaniceotto/bugfix/uDotParachute
# Bug Fixes - Fixed bug where air density was always equal to 1.0 for parachute drag force calculation. # Acknowledgements - Special thanks to Isabela Maria Mendes Lopes for identifying the bug! # Version 0.9.6
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README.md

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Please read [CONTRIBUTING.md](https://github.com/giovaniceotto/RocketPy/blob/master/CONTRIBUTING.md) for details on our code of conduct, and the process for submitting pull requests to us. - **_Still working on this!_**
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## Versioning
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**_Still working on this!_**
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## Authors
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* **Giovani Hidalgo Ceotto**
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This project is licensed under the MIT License - see the [LICENSE.md](https://github.com/giovaniceotto/RocketPy/blob/master/LICENSE) file for details
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## Acknowledgments
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## Release Notes
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Want to know which bugs have been fixed and new features of each version? Check out the [release notes](https://github.com/giovaniceotto/RocketPy/releases).
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**_Still working on this!_**

docs/conf.py

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author = 'Giovani Hdalgo Ceotto'
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# The full version, including alpha/beta/rc tags
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release = '0.9.5'
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release = '0.9.6'
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# -- General configuration ---------------------------------------------------

rocketpy/Flight.py

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freestreamY = vy - windVelocityY
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freestreamZ = vz
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# Determine drag force
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pseudoD = -0.5 * CdS * freestreamSpeed - ka * rho * 4 * np.pi * (R ** 2) * Rdot
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pseudoD = -0.5 * rho * CdS * freestreamSpeed - ka * rho * 4 * np.pi * (R ** 2) * Rdot
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Dx = pseudoD * freestreamX
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Dy = pseudoD * freestreamY
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Dz = pseudoD * freestreamZ

rocketpy/__init__.py

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__copyright__ = "Copyright 20XX, Projeto Jupiter"
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__credits__ = ["Matheus Marques Araujo", "Rodrigo Schmitt", "Guilherme Tavares"]
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__license__ = "MIT"
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__version__ = "0.9.5"
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__version__ = "0.9.6"
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__maintainer__ = "Giovani Hidalgo Ceotto"
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__email__ = "[email protected]"
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__status__ = "Production"

setup.py

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setuptools.setup(
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name="rocketpyalpha",
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version="0.9.5",
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version="0.9.6",
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install_requires = [
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'numpy>=1.0',
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'scipy>=1.0',

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