DATA REPORT: ARNOLD ENGINEERING DEVELOPMENT CENTER TUNNEL C: BOEING COMPANY TEST NO. 005 SURFACE ROUGHNESS HEAT TRANSFER AND PRESSURE TEST ON AD-633M-1 MODEL,

Abstract

Wind tunnel tests were conducted to obtain heat transfer and pressure data from a series of flat plate s with various wave configurations representing surface roughness. The model was tested of angles of attack from -5 to +10 degress. (Author)

Document Details

Document Type
Technical Report
Publication Date
Oct 15, 1963
Accession Number
AD0425510

Entities

People

  • Dwight P. Ayling

Organizations

  • Boeing

Tags

DTIC Thesaurus Topics

  • Energy Transfer
  • Engineering
  • Heat Transfer
  • Physical Properties
  • Roughness
  • Surface Roughness
  • Wind Tunnel Tests
  • Wind Tunnels

Readers

  • Aerodynamics/Aeronautics.
  • Combustion and Flow Dynamics.