Force and Pressure Tests of a Six Caret-Wing-Body Model,

Abstract

Tests to determine six-component force and pressure distribution data on a six caret-wing-body model were performaned in a hypersonic shock tunnel. The report presents the details of the test program, a description of the model and equipment used, and a tabular and graphic presentation of obtained data.

Document Details

Document Type
Technical Report
Publication Date
Feb 20, 1968
Accession Number
AD0759708

Entities

People

  • G. K. Mruk

Organizations

  • Calspan

Tags

DTIC Thesaurus Topics

  • Blast Tubes
  • Buildings And Structures
  • Pressure Distribution
  • Shock Tunnels
  • Test Equipment

Fields of Study

  • Physics

Readers

  • Computer Science.
  • Fluid Dynamics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flight
  • Hypersonics - Hypersonic Flow