Major decisions taken and some of timing aspects and testing involved in development of aircraft, planned as shorter range lower direct operating cost companion to Boeing 707; problem of short range jet operating at lower altitudes and spending larger percent of its time climbing and descending, than long range aircraft; attainment of smooth ride under these conditions demands appropriate cruise wing loading and wing sweepback; body cross section and length, number of engines, engine placement, and other considerations; controls and autopilot; testing programs.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Development of Boeing 727


    Additional title:

    Roy Aeronautical Soc -- J


    Contributors:

    Published in:

    Publication date :

    1963


    Size :

    8 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




    MAG-transit Development at boeing

    Gilliland, R.G. | Tema Archive | 1979


    Boeing 234 flight control development

    Morris, J. J. | NTRS | 1982


    Boeing

    Online Contents | 2012


    Boeing stress analysis workstation development

    JACK, D. / GAMA-LOBO, F. | AIAA | 1985


    Boeing

    Online Contents | 2007