Non-intrusive flow diagnostics for unsteady inlet flow distortion measurements in novel aircraft architectures

Inlet flow distortion is expected to play a major role in future aircraft architectures where complex air induction systems are required to couple the engine with the airframe. The highly unsteady distortions generated by such intake systems can be detrimental to engine performance and were previous...

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Veröffentlicht in:	Progress in aerospace sciences 2022-04, Vol.130, p.100810, Article 100810
Hauptverfasser:	Doll, Ulrich, Migliorini, Matteo, Baikie, Joni, Zachos, Pavlos K., Röhle, Ingo, Melnikov, Sergey, Steinbock, Jonas, Dues, Michael, Kapulla, Ralf, MacManus, David G., Lawson, Nicholas J.
Format:	Artikel
Sprache:	eng
Schlagworte:	Air induction systems Aircraft Aircraft design Aircraft stability Airframes Complexity Convoluted diffusers Cross flow Filtered Rayleigh Scattering (FRS) Flow distortion Flow stability Fuselages Inlet flow Inlet flow distortion Intake systems Laser based flow measurements Measurement methods Non-intrusive flow diagnostics Propulsion integration Rayleigh scattering Seeding-free measurements Spatial resolution Static pressure Unsteady flow
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