Static and Dynamic Stability Characteristics of the Fixed-Fin and Inflatable Stabilizer Retarder Configurations of the MK-82 Store at Transonic Speeds

Abstract

An investigation was conducted in the Aerodynamic Wind Tunnel (4T) to obtain the static stability and pitch-damping characteristics of the Fixed-Fin (FF) and Inflatable Stabilizer Retarder (ISRe) configurations of the MK-82 store with solid and slotted fins and with various fin tabs. The static phase was conducted using 0.20-scale models, and the dynamic phase was conducted using 0. 442-scale models. The tests were conducted at Mach numbers from 0.4 to 1.3 for angles of attack up to 42 deg and Reynolds numbers from 200,000 to 1,000,000 based on the centerbody maximum diameter. All configurations tested were statically and dynamically stable. The ISRe configurations had a greater static stability margin than the FF configurations. Use of the slotted fin reduced the static stability margin of the FF configurations but had no significant effect on the ISRe configurations. The slotted fin had little or no effect on the dynamic stability characteristics. Increasing fin tab angle generally caused an increase in dynamic stability for subsonic Mach numbers and a decrease for supersonic Mach numbers. The dynamic stability generally increased with increasing angle of attack.

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Document Details

Document Type
Technical Report
Publication Date
Nov 01, 1975
Accession Number
ADB007733

Entities

People

  • C. F. Anderson
  • W. E. Carleton

Organizations

  • Arnold Engineering Development Complex

Tags

Communities of Interest

  • Air Platforms
  • Materials and Manufacturing Processes

DTIC Thesaurus Topics

  • Acquisition
  • Aerodynamic Characteristics
  • Aerodynamic Forces
  • Air Force
  • Data Acquisition
  • Diameters
  • Dynamic Pressure
  • Instrumentation
  • Mach Number
  • Measurement
  • Moment Of Inertia
  • Resonant Frequency
  • Reynolds Number
  • Scale Models
  • Test And Evaluation
  • Test Facilities
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow