An experimental setup has been developed to study the wing-nacelle interaction of commercial transports during transonic operation. This stand allows the measurement of the overall loads, pressure distribution on the model, and velocities in the field by laser velocimetry. The analysis gives a better understanding of the wing-nacelle interaction and provides the best comparative elements for modeling calculations.
Analyse Detaillee de l'Interaction Voilure-Nacelle d'UN Avion de Transport Civil (Detailed Analysis of Wing-Nacelle Interaction for Commercial Transport Aircraft)
1992
11 pages
Report
Keine Angabe
Englisch
Aerodynamics , Aircraft , Flow distribution , Interactional aerodynamics , Transport aircraft , Wind tunnel tests , Wing nacelle configurations , Commercial aircraft , Aerodynamic loads , Flow velocity , Laser doppler velocimeters , Pressure distribution , Transonic flight , Wind tunnel models , Foreign technology
Nacelle-wing integration aspects for the high-speed civil transport aircraft
British Library Conference Proceedings | 1995
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