Preparatory to developing mission profiles for future attack, crane, observation, assault, transport, and utility helicopters, the flight condition recognition (FCR) technique was applied to some 10-hour data samples for each of the following class-model helicopters which had acquired 200 or more hours of multichannel oscillograph data during operational usage surveys while the helicopters operated under combat conditions in Southeast Asia (SEA): attack - AH-1G, crane - CH-54A, observation - OH-6A, assault - UH-1H, transport - CH-47A, and utility - UH-1H.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Dynamic Loads and Structural Criteria


    Contributors:
    T. L. Cox (author) / R. B. Johnson (author) / S. W. Russell (author)

    Publication date :

    1975


    Size :

    200 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Dynamic Loads and Structural Criteria Study

    K. R. Spreuer / S. J. Snackenburg / G. D. Roeck | NTIS | 1974




    Thermal-Structural Combined Loads Design Criteria Study

    V. Deriugin / E. W. Brogren / C. L. Jaeck et al. | NTIS | 1972


    Thermal-structural combined loads design criteria study

    Deriugin, V. / Brogren, E. W. / Jaeck, C. L. et al. | NTRS | 1972