A simulation study was conducted to determine the effect of wind shear on aircraft landings. The landing of various type of commercial and military aircraft was digitally simulated starting from an initial altitude of 300 feet. Assuming no pilot feedback during descent, the deviation in touchdown point due to vertical profiles of wind shear was determined. The vertical profiles of wind shear are defined in terms of surface roughness, Z sub 0, and stability, L, parameters. The effects on touchdown due to Z sub 0 and L have been calculated for the different type aircraft. Comparisons were made between the following types of aircraft: (1) C-130E, (2) C-135A, (3) C-141, (4) DC-8, (5) Boeing 747, and (6) an augmentor-wing STOL. In addition, the wind shear effect on touchdown resulting from different locations of the center of gravity and gross weights was also analyzed.


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    Titel :

    Effect of shear on aircraft landing


    Beteiligte:
    Luers, J. K. (Autor:in) / Reeves, J. B. (Autor:in)

    Erscheinungsdatum :

    01.07.1973


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Effect of Shear on Aircraft Landing

    J. K. Luers / J. B. Reeves | NTIS | 1973


    Effect of shear on aircraft landing

    Luers, James K. / Reeves, Jerry B. | TIBKAT | 1973


    Wind Shear Effects on the Landing of Aircraft

    James K. Luers / Jerry B. Reeves | AIAA | 1975


    Control of aircraft landing approach in wind shear

    Chu, Peter Yaohwa / Bryson, Arthur E., Jr. | NTRS | 1987


    Control of aircraft landing approach in wind shear

    CHU, PETER / BRYSON, JR., ARTHUR | AIAA | 1987