PROPOSED INVESTIGATION OF VISCOUS-INVISCID EFFECTS IN HYPERSONIC FLOW IN THE AEDC GAS DYNAMICS FACILITY TUNNEL B-2. PHASE I
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 (S/R) equal to 1.22 instrumented for pressure and heat transfer on upper and lower surfaces.
Document Details
- Document Type
- Technical Report
- Publication Date
- Oct 01, 1959
- Accession Number
- AD0256170