Numerical Modeling of Helicopter Main Rotor Behavior near a Small-Scale Helideck by the Vortex Method

Author:

Aparinov A. A.,Kritskii B. S.,Setukha A. V.

Publisher

Allerton Press

Subject

Aerospace Engineering

Reference13 articles.

1. Belotserkovskii, S.M., Loktev, B.E., and Nisht, M.I., Issledovanie na EVM aerodinamicheskikh i aerouprugikh charakteristik vintov vertoletov (Computer-Aided Study of Aerodynamic and Aeroelastic Characteristics of the Helicopter Rotors), Moscow: Mashinostroenie, 1992.

2. Borisov, E.A., Leont’ev, V.A., Rubinstein, M.A., Sokolov, S.V., and Tarasov, N.N., Experimental Study of the Influence of Platforms of Limited Size on the Aerodynamic Helicopter Performance, Proc. of 10th Forum of Russian Helicopter Society, Moscow: RosVO, 2012, pp. 32–41.

3. Liss, A.Yu., Approximate Technique of Tip Vortex Account in Calculating a Helicopter Main Rotor, Izv.Vuz. Av. Tekhnika, 2012, vol. 55, no. 2, pp. 19–23 [Russian Aeronautics (Engl. Transl.), vol. 55, no. 2, pp. 136–143].

4. Garipova, L.I., Batrakov, A.S., Kusyumov, A.N., Mikhailov, S.A., and Barakos, G.N., Estimates of Hover Aerodynamics Performance of Rotor Model, Izv.Vuz. Av. Tekhnika, 2014, vol. 57, no. 3, pp. 7–13 [Russian Aeronautics (Engl. Transl.), vol. 57, no. 3, pp. 223–231].

5. Belotserkovskii, S.M. and Nisht, M.I., Otryvnoe i bezotryvnoe obtekanie tonkikh kryl’ev ideal’noi zhidkost’yu (Separated and Separation-Free Flows of Ideal Fluid around Thin Wings), Moscow: Nauka, 1978.

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