Examples of structures include conventional sheet-stringer panels, honeycomb panels, integrally machined and stiffened panels, trusscore panels and others; separate Zee stiffeners attached to thin skin are fabricated at low cost and have reasonable efficiencies; integrally machined and honeycomb panels are more efficient, and also are more expensive to fabricate; therefore, aerospace engineer is constantly seeking means of obtaining improved panel concepts that result in higher structural efficiency at lower manufacturing costs.
Comparison of integrally formed compression panel efficiencies with other aerospace panel concepts
AIAA-ASME Structures, Structural Dynamics Matls Conference
8th AIAA-ASME Structures, Structural Dynamics and Materials Conference ; 1967 Stresses
1967
9 pages
Aufsatz (Konferenz)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.