PROPOSED INVESTIGATION OF VISCOUS-INVISCID EFFECTS IN HYPERSONIC FLOW IN THE AEDC GAS DYNAMICS FACILITY TUNNEL B-2. PHASE I
GENERAL APPLIED SCIENCE LABS INC HEMPSTEAD N Y
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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.