A Wind Tunnel Evaluation of an FMU-110B Fuze Mounted on an SUU-30 Dispenser at Mach Numbers from 0.20 to 1.40

Abstract

Results are presented of a wind tunnel evaluation of an FMU-110B fuze which was mounted on the radome protruding from the nose of an SUU-30 bomb dispenser (full scale). The test was conducted at Mach numbers from 0.20 to 1. 40, at angles of attack from -10 to 10 deg, and at roll angles from 0 to 180 deg.

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Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1975
Accession Number
ADB003672

Entities

People

  • J. A. Collins

Organizations

  • Arnold Engineering Development Complex

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Dispensers
  • Dynamic Pressure
  • Engineering
  • Free Stream
  • Government Procurement
  • Governments
  • Instrumentation
  • Mach Number
  • Measurement
  • Pressure Distribution
  • Pressure Measurement
  • Static Pressure
  • Test And Evaluation
  • Test Facilities
  • United States
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Organizational Process Management (OPM).