WIND TUNNEL TEST OF A SELF-ALIGNING SPIKE.

Abstract

The spike protected dome concept for supersonic odies has previously been demonstrated to be a promising technique for protection against rain erosion as well as reducing drag, aerodynamic and structural loading. It is desirable, however, that the spike be aligned with the oncoming flow such that a uniform flow separation region may be maintained over the dome. Towards a solution to this problem the self-aligning spike system automatically maintains spike alignment with the airstream using a self-contained unit which requires no external power. This system has now been demonstrated at M = 5.0. The results show that spike alignment in the airstream may be maintained within plus or minus 3 deg up to an angle of attack of 20 deg. Natural frequencies of the system were well beyond the natural frequencies of typical missiles.

Document Details

Document Type
Technical Report
Publication Date
May 01, 1966
Accession Number
AD0488618

Entities

People

  • James E. Nicholson
  • Joseph J. Rossi
  • Richard H. Adams

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Flow
  • Flow Separation
  • Frequency
  • Rain Erosion
  • Resonant Frequency
  • Wind Tunnel Tests
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Structural Dynamics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow