Inapropはプロペラ設計プログラムです。 渦法、Larrabeeの手法、Adkins & Liebeckの手法それぞれによる設計が可能です。 v0.55の現在、十分な機能が実装されておらず、バグが残っているために、 それぞれの手法のアルゴリズムサンプルとして使ってもらえると思います。 プロペラ設計プログラムとしてはXROTORという優れたオープンソースプログラムが存在しています。 ちゃんと使いたかったらそちら推奨です。
実行ファイルはbin\Relese\Inaprop.exeです.ソースコードのダウンロードやインストールの必要はありません.
Inaprop is GUI propgram for the design and analysis of free-tip propellers. Inaprop has three design methods which are Vortex methos, Larrabee method and Adkins $ Liebeck method(BEM:Blade Element Momentum method). Analysis routine is not implementation yet. Inaprop function is not enough yet.And there is an excellent rotor desing and analysis software 'XROTOR', please use there.
If you just use, you only need the executable file(bin\Relese\Inaprop.exe)
Microsoft .NET Framework 4 http://www.microsoft.com/ja-jp/download/details.aspx?id=17851
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誘導損失最小のプロペラの設計(Larrabee,Adkins & Liebeckの手法)
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損失最小のプロペラの設計(渦法)
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複数パラメータの設計プロペラのグラフ表示
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etc... その他の機能も実装するかも
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Design of minimum indeced loss propeller(Larrabee, Adkins & Liebeck method)
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Desing of minimum loss propeller(vortex methos)
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Multi-point parameter display
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.... It will be implemented other features.
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原田正志,“低レイノルズ数プロペラの設計法”,宇宙航空研究開発機構研究開発報告 JAXA-RR-06-032, 1-13, 2007-03
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Harada,"Design of propeller in low Reynolds number range",JAXA-RR-06-032, 1-13, 2007-03 http://repository.tksc.jaxa.jp/pl/dr/AA0063471000
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Chattot,"Optimization of propellers using helicoidal vortex model",Computational Fluid Dynamics Journal,2000 http://mae.ucdavis.edu/chattot/publications/jjcoptiprop.pdf
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Larrabee.E.E,"Practical Design of Minimum Induced Loss Propellers,"SAE Technical Paper 790585, 1979, doi:10.4271/790585
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Larrabee, E. E., Practical design of minimum induced loss propellers, SAE Technical Paper 790585, 1979. http://ja.scribd.com/doc/82049292/Minimum-Induced-Loss-Propeller-E-Larrabee
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Design of Propellers for Motorsoarers http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19790015732_1979015732.pdf
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Adkins, C. N., Liebeck, R. H., Design of optimum propellers, Journal of Propulsion and Power, vol. 10 (1994), no. 5, pp 676–682.
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高沢金吾, 外立政隆, 野中修:"低レイノルズ数域のプロペラ風洞試験",航空宇宙技術研究所報告 TR-1071, 1990-06, pp.29-
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TAKASAWA et al,"Wind Tunnel Test of a Propeller Working in a Low Reynolds Number Range"NAL TR-1071, 1990-06, pp.29- http://airex.tksc.jaxa.jp/pl/dr/NALTR1071000
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Betz, A. with Appendix by L. Prandtl, Schraubenpropeller mit Geringstem Energieverlust, Göttinger Nachrichten, Göttingen, 1919, pp 193–217.
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Goldstein, S., On the vortex theory of screw propellers, Proc R Soc London A, 1929, 123, pp. 440–465.
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Wald, Q. R., The aerodynamics of propellers, Progress in Aerospace Sciences 42 (2006), pp 85–128, http://www.sciencedirect.com/science/article/pii/S0376042106000455
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Klesa, "Comparison of Methods for Computtion of Ideal Circulation Distribution on the Propeller" http://stc.fs.cvut.cz/History/2010/Sbornik/papers/pdf/KlesaJan-306748.pdf
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How Propellers Work - Propeller Design Workshop https://www.google.co.jp/url?sa=t&rct=j&q=&esrc=s&source=web&cd=7&cad=rja&ved=0CG0QFjAG&url=http%3A%2F%2Fpropellerdesignworkshop.com%2Ffiles%2FPropeller%2520Design%2520Workshop%2520Part%2520II.pps&ei=81j7UPDRCsLUmAXmooG4Bg&usg=AFQjCNEOKug9Oozhe7p3xia_P4U2ZM0LeQ&sig2=_gnGtWiYjG2LWUlnHwj9OA
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my blog http://www.ina111.org
Copyright (c) 2013 Inagawa Takahiro Inaprop is Licensed under MIT License. You may copy, modify and redistribute Inaprop or its modifications freely. The code has been developped exclusively for design propeller in low reinolds number region. All other usages are strongly disapproved. Inaprop is released free, without any guarantee of any kind. Design of all products with the use of the code will be at the user's entire risk Inaprop is by no means a professional product, and does not offer the same gurantees of robustness, reliability, precision or product support than commercial softwares.