Low Density Boundary Layer Modulation By Suction In A Hypersonic Nozzle
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Author | : Max Kinslow |
Publisher | : |
Total Pages | : 40 |
Release | : 1973 |
Genre | : Hypersonic wind tunnels |
ISBN | : |
The potential value of controlled boundary-layer removal from the wall of a nozzle for low-density hypersonic flow was investigated in a brief experimental program. A particular objective was the achievement of sufficient control over boundary-layer thickness to enable a contoured nozzle to be operated under off-design conditions without excessive deterioration of flow uniformity. The nozzle contour was greatly influenced by boundary-layer thickness. Boundary-layer removal involved suction through perforated walls where local nozzle static pressures exceeded the pressure in the large tank which enclosed the nozzle and test section.
Author | : |
Publisher | : |
Total Pages | : 0 |
Release | : 1972 |
Genre | : |
ISBN | : |
The potential value of controlled boundary-layer removal from the wall of a nozzle for low-density hypersonic flow was investigated in a brief experimental program. A particular objective was the achievement of sufficient control over boundary-layer thickness to enable a contoured nozzle to be operated under off-design conditions without excessive deterioration of flow uniformity. The nozzle contour was greatly influenced by boundary-layer thickness. Boundary-layer removal involved suction through perforated walls where local nozzle static pressures exceeded the pressure in the large tank which enclosed the nozzle and test section. (Author).
Author | : |
Publisher | : |
Total Pages | : 0 |
Release | : 1972 |
Genre | : |
ISBN | : |
The potential value of controlled boundary-layer removal from the wall of a nozzle for low-density hypersonic flow was investigated in a brief experimental program. A particular objective was the achievement of sufficient control over boundary-layer thickness to enable a contoured nozzle to be operated under off-design conditions without excessive deterioration of flow uniformity. The nozzle contour was greatly influenced by boundary-layer thickness. Boundary-layer removal involved suction through perforated walls where local nozzle static pressures exceeded the pressure in the large tank which enclosed the nozzle and test section. (Author).
Author | : |
Publisher | : |
Total Pages | : 548 |
Release | : 1995 |
Genre | : Aeronautics |
ISBN | : |
Author | : David L. Whitfield |
Publisher | : |
Total Pages | : 12 |
Release | : 1969 |
Genre | : Aerodynamics, Hypersonic |
ISBN | : |
Author | : David E. Boylan |
Publisher | : |
Total Pages | : 68 |
Release | : 1973 |
Genre | : Aerodynamic heating |
ISBN | : |
The report presents heat-transfer-rate measurements on sharp and blunt 10-deg half-angle cones at angles of attack between -9 and +10 deg 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).
Author | : |
Publisher | : |
Total Pages | : 1964 |
Release | : 1964 |
Genre | : Aeronautics |
ISBN | : |
Author | : Dennis M. Bushnell |
Publisher | : |
Total Pages | : 44 |
Release | : 1969 |
Genre | : Aerodynamics, Hypersonic |
ISBN | : |
Turbulent boundary layer measurements on axisymmetric hypersonic nozzle walls.
Author | : Serge A. Waiter |
Publisher | : |
Total Pages | : 44 |
Release | : 1960 |
Genre | : Aerodynamics, Hypersonic |
ISBN | : |
Author | : Mitchel H. Bertram |
Publisher | : |
Total Pages | : 40 |
Release | : 1959 |
Genre | : |
ISBN | : |