RAIN EROSION ON SPIKE-PROTECTED SUPERSONIC RADOMES

Abstract

This report describes a sled test and shock tube test program designed to assess the effectiveness of flow separation devices in providing rain erosion protection to missile radomes. In the sled test program models were run at supersonic speeds through heavy rain. Those models with the flow separating device sustained little or no damage whereas unprotected models were totally destroyed by rain erosion. In the shock tube, drop breakup was studied over a wide range of the basic scaling parameters. Correlation of the shock tube data with previous drop breakup theory and extension of this theory to the sled test conditions yields results in excellent agreement. These results are then used to predict flow separation configurations at other altitudes and velocities of interest. Based on the results of these two experimental programs and the follow-up analysis, it may be concluded that flow separation techniques are an effective solution to the problem of rain erosion at supersonic speeds.

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Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1965
Accession Number
AD0363299

Entities

People

  • Jacques A. F. Hill
  • James E. Nicholson

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Altitude
  • Boundary Layer
  • Dynamic Pressure
  • Erosion
  • Flight Speeds
  • Flow
  • Fluid Dynamics
  • Mach Number
  • Pressure Distribution
  • Rain Erosion
  • Shock Tubes
  • Sled Tests
  • Test Equipment
  • Test Facilities
  • Tubes
  • Turbulent Mixing
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Coastal and Marine Engineering/Sediment Transport/Hydraulic Engineering
  • Fluid Dynamics.
  • Radar Systems Engineering.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow