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

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.

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1965
Accession Number
AD0640338

Entities

Organizations

  • General Electric

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Actuators
  • Aircrafts
  • Airframes
  • Engines
  • Fans
  • Flight
  • Fuselages
  • Hydraulic Actuators
  • Jet Engines
  • Lift Fans
  • Materials
  • Research Aircraft
  • Stress Analysis
  • Structural Analysis

Fields of Study

  • Physics

Readers

  • Aerodynamics.
  • Aerodynamics/Aeronautics.