Advanced In-flight Measurement Techniques

AIM

The research project Advanced In-flight Measurement Techniques (AIM) intends to develop advanced non-intrusive in-flight measurement techniques for efficient, cost-effective in-flight testing for certification and in-flight research for aircraft and helicopters.  In order to achieve this ambitious goal AIM will organize and structure a close collaboration among leading experts from industry, research organizations, universities and an SME with complementary knowledge and experience of in-flight testing, development of image based measurement techniques and operation of small airports.

 Partner Organisation

Acronym

Country Code

 Deutsches Zentrum für Luft- und Raumfahrt e.V.

 DLR

 DE

 AIRBUS France

 A-F

 FR

 Eurocopter Deutschland

 EC-D

 DE

 Eurocopter SAS

 EC-F

 FR

 Piaggio

 Piaggio

 IT

 EVEKTOR

 EVEKTOR

 CZ

 Stichting Nationaal Lucht- en Ruimtevaartlaboratorium

 NLR

 NL

 Office National d’Études et de Recherches Aérospatiales

 ONERA

 FR

 Cranfield University

 Cranfield

 GB

 Moscow Power Engineering Institute (Technical University)

 MPEI(TU)

 RU

 Flughafen Braunschweig

 FB

 DE

Proposal abstract

The design of a new aircraft as well as the modification of existing types requires comprehensive numerical and experimental studies. The results of the design process and thus the definitive quality of the product will be verified during flight tests for certification. Extrapolating data obtained in the wind tunnel or at low Reynolds number simulations to real flight is not trivial and primarily based on engineering experience, sometimes exhibiting considerable deviations from the predictions. In terms of measurement techniques non-intrusive optical image based methods have undergone considerable technological progress during the past decade. These techniques shall be further developed such that they can be routinely applied to flight tests to provide comprehensive planar information on various important parameters such as wing and propeller deformation, thermal loads on the structure of helicopters, the planar pressure distribution on a wing, density gradients of strong vortices generated by airplanes and helicopters and velocity flow fields near airplanes and helicopters. The main emphasis will be on development of methods requiring little or no modifications to existing aircraft. The development will be done by progressive stages, from initial tests with ground based instrumentation, to in-flight feasibility studies and final validation tests of the most promising measurement techniques on a large transport aircraft, a helicopter and a light aircraft. The AIM partnership comprises the flight testing departments of five industrial partners which manufacture transport airplanes, helicopters and light airplanes, three research organizations with expertise in advanced measurement techniques and flight testing and two partners from universities with expertise in measurement techniques (one of them from a NIS country and the other with knowledge on flight testing), and a small enterprise operating an airport which is frequently used for flight testing.


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