Accession Number:

AD0256170

Title:

PROPOSED INVESTIGATION OF VISCOUS-INVISCID EFFECTS IN HYPERSONIC FLOW IN THE AEDC GAS DYNAMICS FACILITY TUNNEL B-2. PHASE I

Descriptive Note:

Corporate Author:

GENERAL APPLIED SCIENCE LABS INC HEMPSTEAD N Y

Personal Author(s):

Report Date:

1959-10-01

Pagination or Media Count:

1.0

Abstract:

This report includes NOTE ON B-2 DATA REDUCTION. SUPPLEMENT TO TM-26. Oct 59. 3p. incl. table.A test program is presented for a series of hypersonic research tests to provide detailed data for pressure distribution and heat transfer over several model configurations. The following configurations are to be studied 1 spherically blunted cone instrumented for pressure distribution 2 spherically blunted cone instrumented for heat transfer measurement 3 2-dimensional flat plate with 0.1-in. leading edge radius instrumented for simultaneous measurement of pressure and heat transfer on windward surface 4 2-dimensional flat plate with 0.5-in. leading edge radius instrumented for pressure and heat transfer measurement on windward surface and in the vicinity of the nose region and 5 2-dimensional flat plate with 0.5-in. leading edge radius with planes tangent to body at sonic point and tangent SR equal to 1.22 instrumented for pressure and heat transfer on upper and lower surfaces.

Subject Categories:

Distribution Statement:

APPROVED FOR PUBLIC RELEASE