Accession Number:

ADA416231

Title:

Enhancement to Repair Assessment Procedure and Integrated Design (RAPID). Analysis Methods Enhancements

Descriptive Note:

Final rept. 1 Nov 1998-31 May 2000

Corporate Author:

BOEING CO LONG BEACH CA

Personal Author(s):

Report Date:

2000-06-01

Pagination or Media Count:

319.0

Abstract:

This document describes the technical details of the analysis methodology used in the static and damage tolerance analysis modules of the Repair Assessment Procedure and Integrated Design RAPID program. In this document, the static strength analysis method for repaired fuselage skin and skin modifications to antenna installation is first described. Next, a description of the damage tolerance method is provided. This document also includes descriptions of the methods developed for the damage tolerance analysis of common repairs including a repair near another repair and repairs at stiffeners. Flowcharts of static and damage tolerance analysis methods are provided.

Subject Categories:

  • Computer Programming and Software
  • Mechanics
  • Aircraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE