Static Stability and Control Effectiveness of the Super HOBOS/MK-84 (EOGB-II) Munition at Mach Numbers from 0.4 to 1.6

Abstract

Wind tunnel tests were conducted on a 0.25-scale model to determine the static stability and control characteristics of the Super HOBOS/MK-84 (EOGB- II) munition. The tests were performed in the Aerodynamic Wind Tunnel (4T) over a Mach number range from 0.4 to 1.6 at angles of attack from -4 to 26 deg. Aerodynamic coefficients and control effectiveness data are presented. Two techniques, one using multiple flap deflections and the other single flap deflections, were employed during the test. A comparison of the two methods is presented and the results are discussed.

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Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1974
Accession Number
AD0921329

Entities

People

  • D. K. Smith

Organizations

  • Arnold Engineering Development Complex

Tags

DTIC Thesaurus Topics

  • Air Force
  • Angle Of Attack Indicators
  • Calibration
  • Control Surfaces
  • Control Systems
  • Engineering
  • Flaps (Control Surfaces)
  • Indicators
  • Instrumentation
  • Mach Number
  • Measurement
  • Pressure Measurement
  • Surfaces
  • Test And Evaluation
  • Test Facilities
  • Test Methods
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.