Wind Tunnel Evaluation of High Altitude Temperature Sensors.

Abstract

Results of wind tunnel testing of three rocketsonde temperature sensors at reduced pressures are reported. These tests were performed to evaluate the effective aerodynamic recovery factor in rarefied flows simulating flight conditions experienced in rocketsonde flights between 50 and 70 km. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1968
Accession Number
AD0770490

Entities

People

  • K. W. Rogers

Tags

DTIC Thesaurus Topics

  • Altitude
  • High Altitude
  • Recovery
  • Test And Evaluation
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Fluid Dynamics.