?url_ver=Z39.88-2004&rft_val_fmt=info%3Aofi%2Ffmt%3Akev%3Amtx%3Adc&rft.relation=http%3A%2F%2Fmiis.maths.ox.ac.uk%2Fmiis%2F250%2F&rft.title=An+interpolation+tool+for+aircraft+surface+pressure+data&rft.creator=Alam%2C+Mahbubul&rft.creator=Almond%2C+Darryl&rft.creator=Budd%2C+Chris&rft.creator=Hill%2C+Andrew&rft.creator=Schwetlick%2C+Hartmut&rft.subject=Aerospace+and+defence&rft.description=Airbus+UK+are+concerned+with+designing+efficient+wings+for+aircraft.+In+the+design+process%2C+the+aerodynamic+load+on+the+wing+is+calculated+for+various+configurations+including+different+Mach+numbers+and+angles+of+attack.+The+aerodynamic+load+is+calculated+from+the+pressure+profile+around+the+wing.+Airbus+use+a+number+of+different+methods+to+calculate+the+pressure%2C+primarily+CFD+calculations+and+wind+tunnel+experiments.+However%2C+experiments+and+calculations+cannot+be+performed+for+all+configurations.%0D%0A%0D%0AAirbus+asked+the+Study+Group+to+investigate+interpolation+methods+which+incorporate+wind+tunnel+and+CFD+data+to+calculate+the+aerodynamic+load+for+many+different+configurations.&rft.date=2007&rft.type=Study+Group+Report&rft.type=NonPeerReviewed&rft.format=application%2Fpdf&rft.language=en&rft.identifier=http%3A%2F%2Fmiis.maths.ox.ac.uk%2Fmiis%2F250%2F1%2FAirbus-InterpolationReport.pdf&rft.identifier=++Alam%2C+Mahbubul+and+Almond%2C+Darryl+and+Budd%2C+Chris+and+Hill%2C+Andrew+and+Schwetlick%2C+Hartmut++(2007)+An+interpolation+tool+for+aircraft+surface+pressure+data.++%5BStudy+Group+Report%5D+++++