X-22A TRI-SERVICE V/STOL AIRCRAFT

Abstract

Design has progressed in the layout and detailing of systems based on Wind Tunnel Test Results. Releases have been made for fabrication and extra design effort was continued in the Flight Control System. Weight Control program effort was continued in the face of slight increases. Reduction of Wind Tunnel data from the 1/6 scale, 1/7 scale, and others models progressed. Test preparations for continued Wind Tunnel model tests were made. The 1/3 scale test has just entered the initial phase. Acoustic Noise Tests were accomplished during the period, which indicated additional testing was necessary. Test Specimen configuration and Test Requirements are being prepared for these continued tests.

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Document Details

Document Type
Technical Report
Publication Date
Oct 15, 1963
Accession Number
AD0442863

Entities

Organizations

  • Bell Aircraft Corporation

Tags

Communities of Interest

  • Air Platforms
  • Human Systems
  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Aircrafts
  • Airframes
  • Cockpits
  • Contractors
  • Contracts
  • Control Systems
  • Landing Gear
  • Manufacturing
  • Short Takeoff Aircraft
  • Shrouded Propellers
  • Simulators
  • Spars
  • Test And Evaluation
  • Wind Tunnel Models
  • Wind Tunnel Tests
  • Wind Tunnels

Readers

  • Aerospace Engineering
  • Mathematics or Statistics
  • Software Engineering