DEVICE AND METHOD FOR MEASURING PARAMETERS DURING FLIGHT TESTS OF AN AIRCRAFT

摘要

A sensor support (1) comprises a rigid insert (2) on which the sensor is installed and a flexible envelope (3) fitted at its bottom face with a double-sided adhesive (5) to bond it to an aircraft structure (4) with adjustment of its shape. Assembly and disassembly are easy and the air flow is only slightly disturbed. This device is applicable to flight test campaigns of aircraft for example to measure the noise or pressure.