Accession Number : AD0636574

Title :   STRUCTURAL ANALYSIS OF WING SECONDARY COMPONENTS

Corporate Author : GENERAL ELECTRIC CO CINCINNATI OH ADVANCED ENGINE AND TECHNOLOGY DEPT

PDF Url : AD0636574

Report Date : Dec 1963

Pagination or Media Count : 107

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.

Descriptors :   *WINGS, AILERONS, DUCTED FANS, RESEARCH AIRCRAFT, STRUCTURAL COMPONENTS, VERTICAL TAKEOFF AIRCRAFT

Subject Categories : V/STOL
      Research and Experimental Aircraft

Distribution Statement : APPROVED FOR PUBLIC RELEASE