The Static Stability Characteristics of Several Cone-Cylinder-Flare-Cylinder Configurations at Mach Numbers 0.4 to 4.5

Abstract

The aerodynamic characteristics of various cone cylinder-flare-skirt configurations were investigated between Mach Numbers 0.4 to 4.5. The Reynolds number range for the tests was from 0.5 to 6.0 million per foot. Data are presented in basic form, along with cross plots, to show the effect of changing various body component shapes.

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Document Details

Document Type
Technical Report
Publication Date
Jun 03, 1963
Accession Number
AD0410974

Entities

People

  • D. J. Spring

Organizations

  • United States Army Aviation and Missile Command

Tags

Communities of Interest

  • Air Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Corporations
  • Engineering
  • Mach Number
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  • Mathematics
  • Measurement
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  • Physics
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  • Pressure Distribution
  • Test Facilities
  • Universities

Fields of Study

  • Physics

Readers

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  • Combustion and Flow Dynamics.