PRESSURE DISTRIBUTION TESTS ON A 60-DEG AND 70-DEG DELTA WING AT MACH NUMBERS 20 TO 22

Abstract

Pressure distribution tests were made on a 60-deg and a 70-deg delta wing with semicylindrical leading edges in Tunnel Hotshot 2 at mach numbers 20-22 and Reynolds numbers per foot of about 300,000. Angle of attack ranged from -10 to +60 deg. (Author)

Document Details

Document Type
Technical Report
Publication Date
Feb 01, 1961
Accession Number
AD0321831

Entities

People

  • A.r. Wallace
  • W.n. Swain

Organizations

  • Arnold Engineering Development Complex

Tags

DTIC Thesaurus Topics

  • Delta Wings
  • Leading Edges
  • Mach Number
  • Pressure Distribution
  • Reynolds Number

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Fluid Dynamics.