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Methodological foundations for helicopter altitude-speed parameter measurement using aerometric information from the main rotor vortex column

  • Aircraft Instruments and Instrumentation Computer Complexes
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Abstract

The informative aerometric parameters of the helicopter main rotor vortex column, the approaches to their description and perception, the mathematical models of algorithms for determining helicopter altitude-speed parameters using the aerometric information from the vortex column are considered.

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References

  1. Alekseev, N.V., Kravtsov, V.G., Nazarov, O.I., et al., New Generation Systems for Measuring Air Parameters, Aviakosmicheskoe Priborostroenie, 2003, no. 8. pp. 31–36.

  2. Kozitsin, V.I., Makarov, N.N., Porunov, A.A., and Soldatkin, V.M., Analysis of the Helicopter’s Air Data System Principles of Construction, Aviakosmicheskoe Priborostroenie, 2003, no. 10, pp. 2–13.

  3. Kaletka, J., Evaluation of the Helicopter Low Airspeed System Lassie, Journal of American Helicopter Society, 1983, vol. 28, no. 4, pp. 35–43.

    Article  Google Scholar 

  4. Kozitsin, V.K., Mathematical Models of Helicopter Air Data System Channels on the Basis of Freely-Oriented Pressure Tube, Izv.Vuz. Av. Tekhnika, 2006, vol. 49, no. 3, pp. 46–49 [Russian Aeronautics (Engl.Transl.). vol. 49, no. 3, pp. 77–85].

    Google Scholar 

  5. Kozitsin, V.K., Algorithmic Support of Helicopter Air Data Systems with the Use of Free-Oriented Pitot-Static Tube, Izv. Vuz. Av. Tekhnika, 2004, vol. 47, no. 4, pp. 52–57 [Russian Aeronautics (Engl.Transl.). vol. 47, no. 4, pp. 77–85].

    Google Scholar 

  6. Klyuev, G.I., Makarov, N.N., Soldatkin, V.M., and Efimov, I.P., Izmeriteli aerodinamicheskikh parametrov letatel’nykh apparatov (Measuring Set of Aerodynamic Flight Vehicle Parameters), Mishin, A.V., Ul’yanovsk: Izd. Ul’yanovsk Gos.Tekh. Univ., 2005.

    Google Scholar 

  7. Braverman, A.S. and Vaintrub, A.P., Dinamika vertoleta: Predel’nye rezhimy poleta (Helicopter Dynamics: Subcritical Flight Regimes), Moscow: Mashinostroenie, 1988.

    Google Scholar 

  8. Petunin, A.N., Metody i tekhnika izmereniya parametrov gazovogo potoka (Methods and Techniques for Measuring Gas Flow Parameters), Moscow: Mashinostroenie, 1972.

    Google Scholar 

  9. GOST (State Standard) 5212-74: Aerodynamic Table. Dynamic Pressures and Air Stagnation Temperature for Speeds from 10 to 4000 km/h. Parameters, 1974.

  10. GOST (State Standard) 4701-81: Standard Atmosphere. Parameters, 1981.

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Authors and Affiliations

  1. Tupolev State Technical University, Kazan, Russia

    V. V. Soldatkin

Authors
  1. V. V. Soldatkin
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Additional information

Original Russian Text © V.V. Soldatkin, 2010, published in Izvestiya VUZ. Aviatsionnaya Tekhnika, 2010, No. 3, pp. 51–56.

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Soldatkin, V.V. Methodological foundations for helicopter altitude-speed parameter measurement using aerometric information from the main rotor vortex column. Russ. Aeronaut. 53, 320–327 (2010). https://doi.org/10.3103/S1068799810030128

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  • DOI: https://doi.org/10.3103/S1068799810030128

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