Requirements of C-5A military cargo include structural capability to sustain abnormally high lateral gust loads, of recovering from upset at limit speed even though horizontal stabilizer is trimmed full airplane nose down, and to provide high degree of reliability; structural design considerations of C-5A empennage as they affected overall design of airplane are presented; details of MADAR (malfunction analysis detection and recording) system which monitors number of subsystems; four independent hydraulic systems supply power for various control surfaces, doors, and other movable devices; analog computer monitors and controls fuel quantity in each of 12 tanks; control system requirements; flutter and fatigue aspects and use of Rational Probability Analysis.


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    Titel :

    Unique design considerations for large "T" tail aircraft


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:

    Kongress:

    SAE Meeting ; 1968 Freight



    Erscheinungsdatum :

    1968


    Format / Umfang :

    12 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Unique Design Considerations for a Large “T” Tail Aircraft

    Wharton, Charles L | SAE Technical Papers | 1968


    Tail wheel design considerations

    Haiduck, A.F. | Engineering Index Backfile | 1933


    Design Considerations for New Large Aircraft

    Jagger, D. H. / Royal Aeronautical Society | British Library Conference Proceedings | 1993


    Aircraft tail and aircraft comprising such aircraft tail

    LI JINYE / WANG QIMIN / WANG LI et al. | Europäisches Patentamt | 2024

    Freier Zugriff

    Wind tunnel test considerations unique to V/STOL aircraft

    Black, E.L. | Engineering Index Backfile | 1968