WIND TUNNEL MEASUREMENTS OF THE AGARD CALIBRATION MODEL B AT TRANSONIC AND SUPERSONIC SPEEDS,

Abstract

This report presents results of an investigation carried out in the Naval Ordnance Laboratory's Supersonic Tunnel Number 1 to determine the aerodynamic characteristics of the AGARD Calibration Model B. Tests were conducted at free-stream Mach numbers ranging from 0.70 to 3.50, at angles of attack from -4 to +10 degrees, over a Reynolds number range from 0.20 times 100to the 6th power to 0.62 times 10 to the 6th power. (Author)

Document Details

Document Type
Technical Report
Publication Date
Sep 14, 1964
Accession Number
AD0451011

Entities

People

  • James B. Eades Jr.

Organizations

  • Naval Ordnance Laboratory

Tags

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Calibration
  • Fluid Dynamics
  • Free Stream
  • Mach Number
  • Measurement
  • Mechanical Properties
  • Munitions
  • Physical Properties
  • Reynolds Number
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Aerospace Test and Evaluation
  • Fluid Mechanics and Fluid Dynamics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow