RESULTS OF STATIC TEST OF A FULL SCALE, WING MOUNTED, TIP TURBINE DRIVEN LIFT FAN

Abstract

Results are presented of static tests of 53 hr duration conducted on the X353-5 ducted fan mounted in a 10% thick wing. Included are: Descriptions of the test vehicle, facility, instrumentation and equipment; test procedures and results; analysis of test results, conclusions AND DISCUSSION OF ANY PROBLEMS ENCOUNTERED; hardware inspection results; and program recommendations.

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1962
Accession Number
AD0285037

Entities

Organizations

  • General Electric

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies
  • Ground and Sea Platforms

DTIC Thesaurus Topics

  • Accuracy
  • Actuators
  • Aircrafts
  • Boundary Layer
  • Exhaust Gases
  • Far Field
  • Leading Edges
  • Load Cells
  • Mach Number
  • Measurement
  • Pressure Distribution
  • Pressure Measurement
  • Sound Pressure
  • Strain Gages
  • Test Facilities
  • Wind Tunnel Tests
  • Wind Tunnels

Readers

  • Aerodynamics.
  • Aerodynamics/Aeronautics.
  • Software Engineering