Compression response of a sandwich fuselage keel panel with and without damage

View on Open Library

Compression response of a sandwich fuselage keel panel with and without damage

by David M. McGowan

No reviews yet

First published: 1997 1 language

Subjects

Fuselages Graphite-epoxy composites Honeycomb cores Sandwich structures Impact damage Composite structures Finite element method

Reviews

Log in or sign up to write a review.

No reviews yet. Be the first!

You Might Also Like

More in Fuselages

Calculation of three-dimensional, inviscid supersonic, steady flows

Calculation of three-dimensional, invisc...

Gino Moretti

Navier-Stokes and potential theory solutions for a helicopter fuselage and comparison with experiment

Navier-Stokes and potential theory solut...

Mark S. Chaffin

Vibro-acoustics modal testing at NASA Langley Research Center

Vibro-acoustics modal testing at NASA La...

Richard S. Pappa

Around Glare

Coen Vermeeren

Water-tunnel study results of a TF/A-18 and F/A-18 canopy flow visualization

Water-tunnel study results of a TF/A-18 ...

Steven A. Johnson

Two-dimensional aerodynamic characteristics of several polygon-shaped cross-sectional models applicable to helicopter fuselages

Two-dimensional aerodynamic characterist...

Henry L. Kelley