NASA NTRS · 19760012988
ILLIAC 4 and lifting surface theory with boundary layer
Abstract
Aerodynamic flutter and a re-written computer program for its study are discussed. Data cover: (1) lifting surface theory with boundary layer, (2) incompressible, two dimensional, unsteady flow with control surfaces, (3) improved unsteady theory, (4) combined transonic airfoil thickness and shear layer thickness effects, and (5) bending-torsion flutter calculations.
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Dowell, E. H.. 1976-04-01. ILLIAC 4 and lifting surface theory with boundary layer. https://ntrs.nasa.gov/citations/19760012988
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