Pressure measurement in a blow-down wind tunnel

Philpott, D.

doi:10.1016/0263-2241(85)90015-6

Cited by 2 publications

(1 citation statement)

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“…Nowadays, in addition to regular test section calibrations [7][8][9], wind tunnel data quality assurance initiatives typically include periodic check standard model testing [10,11], which is primarily intended to verify data reliability and in-test and test-to-test data repeatability [12,13]. In general, standard wind tunnel models are simplified representations of typical aeronautic shapes, such as an airplane, a missile or a re-entry body, with precisely defined geometries and known aerodynamic characteristics.…”

Section: Introductionmentioning

confidence: 99%

Wind Tunnel Testing of ONERA-M, AGARD-B and HB-2 Standard Models at Off-Design Conditions

et al. 2021

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Published results for standard wind tunnel models at non-standard test conditions are quite rare and/or may not be available. It has been found that those results are a useful aid in preparations for a number of wind tunnel tests in the Military Technical Institute (VTI) in Belgrade. Test campaigns of standard models at non-standard conditions are performed to serve as an internal database for future wind tunnel tests in such environments. Those tests, that partially overlap the referenced Mach number and/or angle of attack ranges, are conducted in different VTI’s test facilities; different model sizes and support stings were used. The standard models used in static measurements in VTI, ranging from simple missile shapes and re-entry bodies to complicated airplanes, are briefly described and sample non-standard test results are given. The correlation of the test results among models and facilities has been done with references in the available ranges, and, after confirming a good agreement, it is assumed that the results are also valid in the extended ranges of conditions. These results may be useful for researchers in other wind tunnel facilities and for those who handle CFD tools.

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