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Comparative analysis of light transport aircraft usefulness from the point of view of direct operating cost and fuel consumption

Autorzy
Treść / Zawartość
Identyfikatory
Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
The need to increase speed, range and operational load in air transport is currently more topical than ever and is related to the efficiency of fuel use. Minimisation of costs and fuel consumption is connected with the necessity to analyse the influence of profile and procedures of flights depending on the type of aircraft functioning in the transport system. The main objective of the paper was to develop a method of determining costs and fuel consumption depending on the aircraft type and the profile of transport tasks fulfilled, and then to carry out comparative calculations for various types of aircraft designed for local transport. Based on the comparative analysis of results, conclusions have been formulated concerning the optimum ranges of using aircraft with various types of propulsion and optimum flight profiles.
Rocznik
Strony
19--24
Opis fizyczny
Bibliogr. 21 poz.
Twórcy
autor
autor
  • Department of Aircraft and Aircraft Engines, Rzeszow University of Technology, W. Pola 2, 35-959 Rzeszow, Poland, zbigklep@prz.edu.pl
Bibliografia
  • [1] Standard Method for Estimating Comparative Direct Operating Cost of Turbine Powered Transport Airplanes, Air Transport Association of America, December 1967.
  • [2] Standard Method for the Estimation of Direct Operating Costs of Transport airplane, Society of British Aircraft Constructors, Issue No. 4, 1959.
  • [3] ANDERSON, J.D., Aircraft Performance and Design, McGraw-Hill 1999.
  • [4] BRUSOW, W., Optimal design of multipurpose aircraft, Institute of Aviation Scientific Library, Warsaw 1996 (in Polish).
  • [5] HOWE, D., Aircraft Conceptual Design Synthesis, Wiley Blackwell 2000.
  • [6] JENKINSON, L. R., SIMPKIN, P., RHODES, D., Civil Jet Aircraft Design, AIAA 1999.
  • [7] KLEPACKI Z., The best type choice of aircraft as multi criteria set ordering problem of available types set, III Scientific Symposium “Technical and exploitation problems in pilots education process”, Deblin, 8-10.12.1999, t.1, z . 1, p. 139-148, 1999, (in Polish).
  • [8] KLEPACKI Z., Optimization of light transport aircraft system, Scientific and Research Journal of Western Centre of Ukrainian Transport Academy, МЕТА, Lvov 1997, p. 96-98 (in Russian).
  • [9] KLEPACKI, Z., MAJKA, A., The meaning of task set structure in multipurpose system design, Polish Society of Theoretical and Applied Mechanics, Mechanics in Aviation ML-IX 2000, p. 207-214, Warsaw 2000, (in Polish).
  • [10] MAJKA, A., Airplane parameters choice improving efficiency of air transport company, III Scientific Conference Telematics and Road Traffic Safety TiBRD’03, Katowice-Ustron 2003, (in Polish).
  • [11] PESCHEL M., RIEDEL C., Multi optimization. Making compromise decisions methods in technical problems, Warsaw, WNT 1979 (in Polish).
  • [12] RAYMER D. P., Aircraft Design. A Conceptual Approach, AIAA Education Series, Washington 1989.
  • [13] ROSKAM J., Airplane Design, Part I-VII, The University of Kansas, 1989.
  • [14] STINTON, D., Design of the Airplane, Blackwell Science 1983.
  • [15] TORENBEEK E., Synthesis of Subsonic Airplane Design, Kulwer Academic Publishers, Dordrecht/ Boston/ London 1982.
  • [16] BADJAGIN А. А., JEGER S. М., Airplane Design, Moscow, Maszinostrojenije, 1972, (in Russian).
  • [17] BRUSOW W.S., BARANOW S. К., Optimal design of aircraft, Moscow, Maszinostrojenije, 1989, (in Russian).
  • [18] JEGER, S. М., Automatic airplane design principles, Moscow, Maszinostrojenije, 1986, (in Russian).
  • [19] JEGER, S. M., Airplane Design, Moscow, logos 2005 (in Russian).
  • [20] PIJAWSKIJ S. А., BRUSOW W. S., HWILON Е. А., Optimization of parameters of multipurpose aircraft, Moscow, Maszinostrojenije 1974, (in Russian).
  • [21] TOMASZEWICZ А. L., Construction and economy of airplane, Moscow, Oboronzdat 1960, (in Russian).
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-article-BSL7-0036-0004
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