Accession Number:

AD0640338

Title:

FUSELAGE STRUCTURAL ANALYSIS. VOLUME 4. ENGINE INLET, THRUST SPOILER, PITCH FAN LOUVERS

Descriptive Note:

Corporate Author:

GENERAL ELECTRIC CO CINCINNATI OH ADVANCED ENGINE AND TECHNOLOGY DEPT

Personal Author(s):

Report Date:

1965-03-01

Pagination or Media Count:

48.0

Abstract:

The structural analyses of the engine air inlet, the thrust spoiler installation, and the pitch fan louver installation of the U. S. Army XV-5A Lift Research Aircraft are presented.

Subject Categories:

  • VSTOL
  • Research and Experimental Aircraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE