Print Email Facebook Twitter 2D wall interference assessment using "Calspan Pipes" Title 2D wall interference assessment using "Calspan Pipes" Author Smith, J. Institution National Aerospace Laboratory NLR Date 1985-04-30 Abstract The applicability of a multi-velocity-component static pipe, proposed by CALSPAN ATC, for measuring boundary velocity vector distributions in behalf of wall interference assessment, has been explored in two-dimensional flow. Comparisons with alternative methods to derive the local flow angle from measured pipe pressures as well as analyses of associated wall corrections for a solid- and slotted-wall test section show that this "CALSPAN Pipe" is, potentially a very useful instrument. The arrangement of the, here applied, pressure measurement technique should be improved, however. Subject aerodynamic interferencemeasured boundary cond.subsonic flowtransonic flowairfoilswind tunnel apparatuswind tunnel wallstwo dimensional flowslotted wind tunnelsstatic pressurepipes (tubes)flow measurementflow velocity To reference this document use: http://resolver.tudelft.nl/uuid:59ff6d15-2558-4001-858d-58c396c202a2 Publisher Nationaal Lucht- en Ruimtevaartlaboratorium Access restriction Campus only Source NLR-TR 85065 U Part of collection Aerospace Engineering Reports Document type report Rights (c) 1985 National Aerospace Laboratory NLR Files PDF NLR_TR_85065_U.pdf 21.02 MB Close viewer /islandora/object/uuid:59ff6d15-2558-4001-858d-58c396c202a2/datastream/OBJ/view