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Effect of lip and centerbody geometry on aerodynamic performance of inlets for tilting-nacelle VTOL aircraft
Author(s) -
R. R. Burley
Publication year - 1979
Publication title -
29th aerospace sciences meeting
Language(s) - English
Resource type - Conference proceedings
DOI - 10.2514/6.1979-381
Subject(s) - nacelle , aerodynamics , inlet , aerospace engineering , acoustics , computer science , marine engineering , engineering , physics , mechanical engineering , turbine

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