Review of changes in aircraft design in recent years; problems associated with flight at extremely high speed, development of integral construction, and aircraft designed to fly in high subsonic and supersonic regimes; steel honeycomb sandwich construction and core development; design features of Cranfield project A-60 supersonic airliners to fly at 1450 mph at altitudes between 57,000-65,000 ft, including structure, power plant, pressurization and air conditioners, and fuel system. (see also Aircraft Eng v 34 n 399 May 1962 p 132-9)


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    Title :

    Design trends -- Aircraft


    Additional title:

    Production Engr


    Contributors:
    Newell, A.F. (author) / Howe, D. (author)

    Published in:

    Publication date :

    1962


    Size :

    22 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Design trends -- Aircraft

    Newell, A.F. / Howe, D. | Engineering Index Backfile | 1962


    Aircraft design trends

    Gassner, A.A. | Engineering Index Backfile | 1929


    Aircraft Design Trends

    Newell, A.F. / Howe, D. | Emerald Group Publishing | 1962


    Rotary wing aircraft design trends

    Wachs, M.A. / Rabbot, Jr., J.P. | Engineering Index Backfile | 1964


    Design trends in aircraft engines

    Morley, F.W.W. / Hooker, S.G. | Engineering Index Backfile | 1962