DRAG LOADING ON MODEL TARGETS

Abstract

Measurements of drag forces on model targets were made during Operation Redwing in the spring of 1956. From the force measurements and measurements of the free-stream parameters of side-on and dynamic pressures, drag coefficients were obtained for each of the model configurations under each of the test conditions. Reasonable drag-coefficient correlation was obtained for all of the test models (except spheres) for the field and wind tunnel data. Hence, it was concluded that, for the model sizes used, the field flow conditions approached the steady-state flow conditions of the wind tunnel. The short-duration flow in the shock tube and the flow blockage resulting from the model size obviated the establishment of steady drag conditions in this facility. Thus, only extrapolations can be made to wind-tunnel and field conditions. (Author)

Document Details

Document Type
Technical Report
Publication Date
Dec 14, 1964
Accession Number
AD0357969

Entities

People

  • J. Petes
  • L. Slifer

Organizations

  • Naval Ordnance Laboratory

Tags

DTIC Thesaurus Topics

  • Coefficients
  • Dynamic Pressure
  • Field Conditions
  • Flow
  • Free Stream
  • Measurement
  • Shock Tubes
  • Steady State
  • Test Facilities
  • Tubes
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Explosive Engineering.
  • Fluid Dynamics.