Study carried out at NAE to determine aerodynamic reactions on oscillating wings in hypersonic flows such as encountered in hypersonic gliders or re-entry vehicles; inviscid data were calculated for 2-dimensional wings and experiments undertaken to verify theoretical analysis and to determine effects of viscous flow phenomena; details of helium hypersonic wind tunnel constructed, calibration data and method of free oscillation used; experimental apparatus, model support and instrumentation.
Oscillatory experiments in helium hypersonic wind tunnel
Canada. Nat Research Council -- Aeronautical Report
1962
20 pages
Report
Englisch
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Hypersonic Wind-Tunnel Free-Flying Experiments with Onboard Instrumentation
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