Wind Tunnel Investigation of Cargo Extraction Parachutes in the Wake of a Lockheed C-141B Starlifter Aircraft.

Abstract

Wind tunnel investigations were conducted to probe the wake of a C-141 aircraft in an airdrop configuration. A rake with twelve 5-hole yaw head probes measured velocities at various positions in the wake, and these measurements were used to compute the vorticity of the wake. In addition, motion pictures and force measurements were taken with three differently sized extraction parachute models attached to the model aircraft by three extraction lines of different lengths. Correlation of parachute behavior with the airflow data indicates that the vortex shed by the inboard flaps and the fuselage-wing junction causes an instability in the performance of the smallest parachute models while the performance of the larger parachute models is relatively unaffected. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1982
Accession Number
ADA124523

Entities

People

  • David W Taylor
  • Gregory G. Huson

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Air
  • Aircraft Models
  • Aircrafts
  • Coefficients
  • Deflection
  • Dynamic Pressure
  • Flow
  • Free Stream
  • Fuselages
  • Measurement
  • Models
  • Motion Pictures
  • Pressure Measurement
  • Simulations
  • Static Pressure
  • Subsonic Wind Tunnels
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Aerial Delivery - Logistics and Supply Chain Management.
  • Aerodynamics/Aeronautics.