Vortex flap flow reattachment line and subsonic longitudinal aerodynamic data on 50p0s to 74p0s delta wings on common fuselage View on Open Library

Vortex flap flow reattachment line and subsonic longitudinal aerodynamic data on 50p0s to 74p0s delta wings on common fuselage

by Neal T Frink

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First published: 1983 1 language
Subjects
Airplanes Canard Wings Flaps (Airplanes) Leading edges (Aerodynamics) Wings, Canard

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