Separation Characteristics of the M-117 Retarded Bomb, Finned BLU-1C/B Bomb, and SUU-42/A Dispenser from the A-7D Aircraft at Mach Numbers from 0.33 to 0.95

Abstract

Tests were conducted in the Aerodynamic Wind Tunnel (4T) using 0.05- scale models to investigate the separation characteristics of the M-117 retarded bomb, finned BLU-1C/B bomb, and SUU-42/A dispenser when released from various wing pylon locations on the A-7D aircraft. Captive trajectory data were obtained at Mach numbers from 0.33 to 0.95 at simulated pressure altitudes from 4000 to 7000 ft. The parent-aircraft angle of attack was varied from 1.8 to 12.3 depending on Mach number, climb angle, and simulated altitude. At selected test conditions, parent climb angles of -70 deg were simulated. In general, for the trajectory intervals of the test, most of the stores separated from the parent aircraft without store-to-parent contact.

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Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1971
Accession Number
AD0889893

Entities

People

  • David W. Hill Jr.

Organizations

  • Arnold Engineering Development Complex

Tags

Communities of Interest

  • Air Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Acquisition
  • Air Force
  • Aircraft Models
  • Aircrafts
  • Altitude
  • Control Systems
  • Data Acquisition
  • Digital Computers
  • Dispensers
  • Dynamic Pressure
  • Free Stream
  • Mach Number
  • Models
  • Scale Models
  • Test And Evaluation
  • Test Facilities
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Aerospace Engineering
  • Fluid Dynamics.
  • Rocket Propulsion.