Accession Number:

AD0759708

Title:

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

Descriptive Note:

Corporate Author:

CORNELL AERONAUTICAL LAB INC BUFFALO N Y

Personal Author(s):

Report Date:

1968-02-20

Pagination or Media Count:

189.0

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.

Subject Categories:

  • Aircraft
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE