On drag and lift analysis of transport aircraft from wind tunnel measurements

The determination of drag and lift of transport aircraft from wind tunnel measurements is discussed for compressible as well as incompressible flow. Effects of model support are neglected. No simplifying assumptions on the flow along the test section walls are made. Based on the assumption of correc...

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Veröffentlicht in:Aerospace science and technology 2008-06, Vol.12 (4), p.337-345
1. Verfasser: van der Vooren, J.
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description The determination of drag and lift of transport aircraft from wind tunnel measurements is discussed for compressible as well as incompressible flow. Effects of model support are neglected. No simplifying assumptions on the flow along the test section walls are made. Based on the assumption of correctable wind tunnel flow, balance measurements and wake survey measurements together indicate a way to derive an angle of attack correction towards the in-flight condition. This will require the same level of (sufficient) accuracy for both types of measurements and for the propulsion mass flux. The blockage correction is assumed to be known. Buoyancy correction is briefly discussed. Propulsion is fully taken into account. Wake survey computational postprocessing is treated in detail. It is shown that wake survey measurements can be limited to the wake cross-sectional area.
doi_str_mv 10.1016/j.ast.2006.10.011
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source Elsevier ScienceDirect Journals
subjects Air transportation and traffic
Applied sciences
Drag and lift analysis
Exact sciences and technology
Ground, air and sea transportation, marine construction
Propulsion effect
Transonic flow
Transport aircraft
Wake survey measurements
Wind tunnel measurements
title On drag and lift analysis of transport aircraft from wind tunnel measurements
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