Print Email Facebook Twitter A method for determining 2D wall interference on an aerofoil from measured pressure distributions near the walls and on the model Title A method for determining 2D wall interference on an aerofoil from measured pressure distributions near the walls and on the model Author Smith, J. Institution National Aerospace Laboratory NLR Date 1981-01-31 Abstract A "measured-boundary-condition" method for determining 2D wall interference has been developed. It applies measured "wall" pressure distributions and a model representation to determine the 2D interference flow field associated with the presence of the test section walls. Special attention has been paid to the model representation. The applicability of the method and some remaining questions are demonstrated by means of experimental results. Subject Two dimensional flowSlotted wind tiuinelsWind tunnel wallsInterferenceWall pressureTest chambersTest sectionCorrectionWind tunnel calibrationWind tunnel testsPressure sensorsPressure measurementSupercritical wingsWind tunnel modelsVerification (proving)Prediction analysis techniques To reference this document use: http://resolver.tudelft.nl/uuid:00bbbfd4-f961-4a28-a161-8ca995f2b719 Publisher Nationaal Lucht- en Ruimtevaartlaboratorium Access restriction Campus only Source NLR-TR 81016 U Part of collection Aerospace Engineering Reports Document type report Rights (c)1981 National Aerospace Laboratory NLR Files PDF NLR_TR_81016_U.pdf 21.34 MB Close viewer /islandora/object/uuid:00bbbfd4-f961-4a28-a161-8ca995f2b719/datastream/OBJ/view