Static Stability and Axial Force Coefficients for the 0.125 Scale Model Mark 82 Low Drag Bomb with Closed Snakeye I Fins at Subsonic and Transonic Speeds

Abstract

Static stability and axial force coefficients are presented as a function of angle of attack for the Mk 82 Low Drag Bomb with Snakeye Fins in the closed position. These data were obtained for a Mach number range from 0.6 to 1. 1; an angle of attack range from minus 6 to plus 20 degrees; and, a roll angle range from 0 to 225 degrees in the NOL Supersonic Tunnel No. 1, using a subsonic nozzle. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Sep 17, 1969
Accession Number
AD0863422

Entities

People

  • V. L. Schermerhorn

Organizations

  • Naval Ordnance Laboratory

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Acquisition
  • Base Pressure
  • Data Acquisition
  • Data Reduction
  • Dynamic Pressure
  • Low Drag
  • Mach Number
  • Munitions
  • Ordnance Laboratories
  • Photonic Metamaterials
  • Rdx
  • Scale Models
  • Static Pressure
  • Subsonic Nozzles
  • United States
  • Wind Tunnel Tests
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Aerodynamics.
  • Combustion and Flow Dynamics.
  • Explosive Engineering.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow