TABULATED STABILITY DATA FOR A SERIES OF RING TAIL BODY CONFIGURATIONS AT MACH NUMBERS FROM 0.8 TO 4.5

Abstract

The static stability characteristics of ring tails on a body of revolution has been investigated during a series of wind tunnel tests. Mach numbers varied from 0.8 to 4.5, and ring diameters varied from 1.25 to 2.50 calibers. This report presents a tabulation of the basic results obtained from the tests.

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Document Details

Document Type
Technical Report
Publication Date
Apr 15, 1965
Accession Number
AD0464027

Entities

People

  • Donald V. Rubin

Tags

Communities of Interest

  • Air Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Abstracts
  • Aircrafts
  • Applied Mathematics
  • Contracts
  • Engineering
  • Mach Number
  • Mathematics
  • Mechanics
  • New Jersey
  • New York
  • Physics
  • Physics Laboratories
  • Supersonic Wind Tunnels
  • Test Facilities
  • Trailing Edges
  • Wind Tunnel Tests
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.