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DETERMINING THE INFLUENCE OF OUTSIDE AIR TEMPERATURE ON AIRCRAFT AIRSPEED

Doris Novak ; Department of Aeronautics, Faculty of Traffic and Transport Sciences, University of Zagreb, Zagreb, Croatia
Tomislav Radišić ; Department of Aeronautics, Faculty of Traffic and Transport Sciences, University of Zagreb, Zagreb, Croatia
Izidor Alfirević ; Department of Aeronautics, Faculty of Traffic and Transport Sciences, University of Zagreb, Zagreb, Croatia

Puni tekst: engleski, pdf (292 KB) str. 45-54 preuzimanja: 1.418* citiraj
APA 6th Edition
Novak, D., Radišić, T. i Alfirević, I. (2012). DETERMINING THE INFLUENCE OF OUTSIDE AIR TEMPERATURE ON AIRCRAFT AIRSPEED. Transactions of FAMENA, 36 (3), 45-54. Preuzeto s https://hrcak.srce.hr/89239
MLA 8th Edition
Novak, Doris, et al. "DETERMINING THE INFLUENCE OF OUTSIDE AIR TEMPERATURE ON AIRCRAFT AIRSPEED." Transactions of FAMENA, vol. 36, br. 3, 2012, str. 45-54. https://hrcak.srce.hr/89239. Citirano 18.04.2021.
Chicago 17th Edition
Novak, Doris, Tomislav Radišić i Izidor Alfirević. "DETERMINING THE INFLUENCE OF OUTSIDE AIR TEMPERATURE ON AIRCRAFT AIRSPEED." Transactions of FAMENA 36, br. 3 (2012): 45-54. https://hrcak.srce.hr/89239
Harvard
Novak, D., Radišić, T., i Alfirević, I. (2012). 'DETERMINING THE INFLUENCE OF OUTSIDE AIR TEMPERATURE ON AIRCRAFT AIRSPEED', Transactions of FAMENA, 36(3), str. 45-54. Preuzeto s: https://hrcak.srce.hr/89239 (Datum pristupa: 18.04.2021.)
Vancouver
Novak D, Radišić T, Alfirević I. DETERMINING THE INFLUENCE OF OUTSIDE AIR TEMPERATURE ON AIRCRAFT AIRSPEED. Transactions of FAMENA [Internet]. 2012 [pristupljeno 18.04.2021.];36(3):45-54. Dostupno na: https://hrcak.srce.hr/89239
IEEE
D. Novak, T. Radišić i I. Alfirević, "DETERMINING THE INFLUENCE OF OUTSIDE AIR TEMPERATURE ON AIRCRAFT AIRSPEED", Transactions of FAMENA, vol.36, br. 3, str. 45-54, 2012. [Online]. Dostupno na: https://hrcak.srce.hr/89239. [Citirano: 18.04.2021.]

Sažetak
Errors that occur in conventional measurement instruments connected to a pitot-static system affect the accuracy and reliability of indicating the basic navigation elements required for the safety of flight. This paper is to present the manner and methods of preparing and implementing experimental measurements in order to determine the stochastic and functional laws of deviation and change in the actual aircraft flying speed with the changes in altitude and airspeed, as well as to determine the influence of the change in air temperature on the measured values of airspeed up to the pressure altitude of 5,000 m. Using a comparative analysis of parameters measured during the flight by means of a sensor system on a twin-engine turboprop aircraft Antonov AN-32 and by means of a GPS instrument as well as theoretical calculations of pressure obtained in accordance with the measured values, this paper will present the problems of measuring the parameters by a pitot-static system.

Ključne riječi
Pitot-static system; air temperature; aircraft speed

Hrčak ID: 89239

URI
https://hrcak.srce.hr/89239

Posjeta: 1.612 *