Laminar Heat Transfer on Sharp and Blunt Ten-Degree Cones in Conical and Parallel Low-Density Flow.

摘要

The report presents heat-transfer-rate measurements on sharp and blunt 10-deg half-angle cones at angles of attack between -9and +10deg in a low-density,hypersonic wind tunnel. Circumferential and longitudinal distributions are presented for cold wall conditions for a range at Mach and Reynolds numbers. The effect of source-like flows was studied by utilizing both conical and contoured expansion nozzles with the same free-stream similarity parameters and model wall temperatures. Comparisons are made with previously published experimental and theoretical results. (Author)