Investigations of Ablation Surface Cross-Hatching.

Abstract

The Ablation-Surface Cross-Hatching Program is one of several programs directed toward understanding and suppressing cross-hatched patterns on ablating surfaces. It consists of two wind tunnel studies with analyses which are reported herein: First, an investigation of the phasing of the pressure and temperature distributions over a two-dimensional nonablating wavy wall confirmed in-house theoretical predictions. It is believed this is the first time that heat transfer and insulated wall temperature phasing correspondence to pressure in the cross-hatching process has been theoretically proved and experimentally confirmed. An unexpected cusping of pressure was found at transonic speeds. Second, hypersonic wind tunnel tests, including six-component force measurements, of conical camphor and Korotherm models extended the cross-hatching angle versus edge Mach number correlation; showed nose tip bluntness effects compatible with this correlation and showed that roll torques produced as a result of windward meridian shift after pattern formation are stable. A pre-cross-hatched nonablating model confirmed cross-hatching experience by indicating higher heat transfer to the valleys than to the ridges.

Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1970
Accession Number
AD0874560

Entities

People

  • Edgar P. Williams
  • George R. Inger

Tags

DTIC Thesaurus Topics

  • Ablation
  • Heat Transfer
  • Hypersonic Wind Tunnels
  • Mach Number
  • Measurement
  • Nose Tips
  • Noses
  • Two Dimensional
  • Wind Tunnel Tests
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Atmospheric Science / Meteorology, specifically Wind Wave Turbulence.
  • Fluid Dynamics.
  • Fluid Mechanics and Fluid Dynamics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers
  • Hypersonics - Hypersonic Flight
  • Hypersonics - Hypersonic Flow
  • Microelectronics
  • Microelectronics - Graphene