Aircraft have greatly changed over the last decades, mainly due to astonishing developments in key technological areas. The present note attempts to correlate the evolution of jet airliners with improvements in aerodynamics and propulsion. A simple model is elaborated from the range equation, taking the main magnitudes of the payload—range diagram as input data. Results show the robustness and potential of such procedures.
Martinez-ValR.On the science of airplane design. In Proceedings of the Giuseppe Gabrielli Centennial Conference, Turin, Italy, 7 October 2003, invited lecture, available on CD-ROM.
10.
Martinez-ValR.PerezE.Optimum cruise lift coefficient in initial design of jet aircraft. J. Aircr., 1991, 29(4), 712–714.
11.
TorenbeekE.Cruise performance and range prediction reconsidered. Prog. Aerosp. Sci., 1997, 33(5–6), 285–321.
12.
BertC. W.Range and endurance of turboprop, turbofan or piston-propelled aircraft having wings with or without camber. Aircr. Des., 1999, 2(4), 183–190.
13.
CavcarM.CavcarA.Comparison of generalized approximate cruise range solutions for turbojet/fan aircraft. J. Aircr., 2003, 40(5), 891–895.
14.
ClarkP.Buying the big jets, 2nd edition, 2007 (Ashgate, Abingdon, UK).
15.
Martinez-ValR.PerezE.AlfaroP.PerezJ.Conceptual design of a medium size flying wing. Proc. IMechE, Part G: J. Aerospace Engineering, 2007, 221(G1), 57–66.
16.
Approximate methods for estimation of cruise range and endurance: aeroplanes with turbo-jet and turbo-fan engines. ESDU 73019, 1973.
17.
Jane's all the world Aircraft,2003 (Jane's, Coulsdon, UK).
18.
Jane's aero-engines, 2005 (Jane's, Coulsdon, UK).
19.
McCormickB. W.Aerodynamics, aeronautics and flight mechanics, 2nd edition, 1995 (John Wiley and Sons, New York).