Skip to Main Content


This article describes the role of the full-scale testing in assessing composite structural systems of aircraft and qualifying them for in-service use. The typical full-scale tests include static, durability, and damage tolerance. The article discusses parameters to consider when developing the basic requirements for the static test. The parameters include material considerations, moisture and temperature effects, structure size, load application alternatives, instrumentation requirements, test procedure considerations, ultimate load requirements, and test results correlation. The basic requirements common for durability and damage tolerance tests, including environmental effects and inspection requirements are also discussed.

You do not currently have access to this chapter.
Don't already have an account? Register

John E. McCarty, Full-Scale Structural Testing, Composites, Vol 21, ASM Handbook, Edited By Daniel B. Miracle, Steven L. Donaldson, ASM International, 2001, p 794–799,

Download citation file:

Close Modal

or Create an Account

Close Modal
Close Modal