Accession Number:

AD0636574

Title:

STRUCTURAL ANALYSIS OF WING SECONDARY COMPONENTS

Descriptive Note:

Corporate Author:

GENERAL ELECTRIC CO CINCINNATI OH ADVANCED ENGINE AND TECHNOLOGY DEPT

Personal Author(s):

Report Date:

1963-12-01

Pagination or Media Count:

107.0

Abstract:

Structural Analysis of the flap, aileron, wing fan closure doors, wing trailing edge, and wing fittings for the U.S. Army XV-5A lift fan research aircraft are presented in this report. For each component, a summary type analysis is presented primarily with the intent of giving structural configuration, final critical loading, and assumptions made. Structural proof tests were conducted satisfactorily on the basic wing, the fan doors, fan fittings, flap and aileron.

Subject Categories:

  • VSTOL
  • Research and Experimental Aircraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE