This AIAA Standard provides a new methodology for assessment of experimental uncertainty and technique for evaluating wind tunnel error sources. The methodolgy is then applied to a force and pressure test. The document is a revision to the original document which was based on a Report of the NATO Advisory Group on Aerospace Research and Development (AGARD).
Product Details
Published: 01/01/1999 ISBN(s): 1563473631 Number of Pages: 86 File Size: 1 file , 480 KB