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Application of panel methods in external store load calculations

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dc.contributor.author Van Den Broek, GJ
dc.date.accessioned 2008-05-09T05:39:32Z
dc.date.available 2008-05-09T05:39:32Z
dc.date.issued 1984-07
dc.identifier.citation Van Den Broek, G. J. 1984. Application of panel methods in external store load calculations. Journal of Aircraft, Vol. 21(7), pp. 537-539. en
dc.identifier.issn 0021-8669
dc.identifier.uri http://hdl.handle.net/10204/2247
dc.description.abstract The effect of aircraft wind modelling on the external store loads is investigated by computing that effect for the external flow field generated by the wing. The application of the panelling /boundary condition method to the perturbation flow field below the wing is first considered; then, the effect of the wing panelling in the leading edge region, where the singularity distributions show large gradients, on the flow field is studied. Both lift and thickness effects are taken into account. en
dc.language.iso en en
dc.publisher American Institute of Aeronautics and Astronautics en
dc.subject Aerodynamic interference en
dc.subject Aerodynamic loads en
dc.subject External stores en
dc.subject Leading edges en
dc.subject Panel method en
dc.subject Wing profiles en
dc.subject Swept wings en
dc.subject Transport aircraft en
dc.subject Unsteady flow en
dc.title Application of panel methods in external store load calculations en
dc.type Article en
dc.identifier.apacitation Van Den Broek, G. (1984). Application of panel methods in external store load calculations. http://hdl.handle.net/10204/2247 en_ZA
dc.identifier.chicagocitation Van Den Broek, GJ "Application of panel methods in external store load calculations." (1984) http://hdl.handle.net/10204/2247 en_ZA
dc.identifier.vancouvercitation Van Den Broek G. Application of panel methods in external store load calculations. 1984; http://hdl.handle.net/10204/2247. en_ZA
dc.identifier.ris TY - Article AU - Van Den Broek, GJ AB - The effect of aircraft wind modelling on the external store loads is investigated by computing that effect for the external flow field generated by the wing. The application of the panelling /boundary condition method to the perturbation flow field below the wing is first considered; then, the effect of the wing panelling in the leading edge region, where the singularity distributions show large gradients, on the flow field is studied. Both lift and thickness effects are taken into account. DA - 1984-07 DB - ResearchSpace DP - CSIR KW - Aerodynamic interference KW - Aerodynamic loads KW - External stores KW - Leading edges KW - Panel method KW - Wing profiles KW - Swept wings KW - Transport aircraft KW - Unsteady flow LK - https://researchspace.csir.co.za PY - 1984 SM - 0021-8669 T1 - Application of panel methods in external store load calculations TI - Application of panel methods in external store load calculations UR - http://hdl.handle.net/10204/2247 ER - en_ZA


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