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[1] Instrukcja Fluenta 6.2.
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[2] Piechna J., Szumowski A.: Prediction of Small Water Drops Separation in Helicopter Engine Diffuser. The Archive of Mechanical Engineering 1995, XLII, vol. 1-2, pp. 19-27.
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[3] Piechna J., Szumowski A.: Numerical Simulation of the Vortex Airfoil Interaction in Transonic Flow. Second Seminar on RDPAE’96, 1996 pp. 29-34.
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[4] Piechna J., Szumowski A.: Effect of miss-distance on the airfoil-vortex interaction Numerical study. Arch. Mech., 50, pp. 127-138, Warszawa 1998.
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[5] Piechna J., Szumowski A.: Effect of Vortex-Strength on the Airfoil-Vortex Interaction. The Archive of Mechanical Engineering 1998, vol. XLV, Nr 1 pp. 31-42.
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[6] Piechna J., Szumowski A.: Numerical study of the parallel vortex airfoil interaction. Academic Computer Center in Gdansk TASK 1998, No 2, pp. 357-372.
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[7] Selerowicz W., Sobieraj G., Szumowski A., Piechna J.: Effect of miss-distance on the airfoil-vortex interaction Experiment. Arch. Mech. 1998, 50, issue 4 pp. 691-701, Warszawa 1998.
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[8] Sobieraj G., Piechna J., Selerowicz W., Szumowski A.: Effect of angle of attack on the airfoil-vortex interaction. The Archive of Mechanical Engineering 1998, vol. XLV, Nr 1 pp. 19-30.
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[9] Ruith M.: Unstructured , Multiplex Rotor Source Model With Thrust And Moment Trimming-Fluent’s VBM Model. Fluent VVV COV TN293, 2005.
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[10] Wirogo S., Ruith M. R.: Fluent in helicopter aerodynamic analysis. Materiały dydaktyczne firmy Fluent.