Airbus Defence and Space is in the process of developing software to optimize the airport take-off and landing-approach paths of their military aircraft for minimum noise impact on nearby communities. Calculation of the noise impact requires computer models of the noise sources on the aircraft, the propagation paths (including possible reflections) and the metric(s) used to quantify the perceived noise on the ground. The main noise sources on the aircraft are typically: jet, engine intake and aerodynamic sources around the landing gear and the airframe. Initially, Airbus used simple analytical models to quantify source strengths and directivities, but in order to get accurate predictions from the models, a test-based calibration must be performed.
In June 2015, Airbus Defence and Space asked Brüel & Kjær to propose a series of fly-over beamforming measurements for calibration of source levels and directivities for their Eurofighter Typhoon fighter jet. The Airbus project leader was Christian Waizmann, and Dr. Ernst Grigat was the technical project coordinator. They had seen our conference papers based on our cooperation with Japan Aerospace Exploration Agency (JAXA) on fly-over beamforming, which describe the use of a microphone array on the ground to localize and quantify noise sources on a passing business jet. A new challenge in connection with the Airbus measurements was the determination of not only source strengths but also their directivities.