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Wind-tunnel investigation of a number of total-pressure tubes at high angles of attack supersonic speeds
1951
2676
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Experimental investigation of two-dimensional tunnel-wall interference at high subsonic speeds
1953
2149
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0
Mach number distributions along the slotted walls of the N.P.L. 20 in × 8 in : Highspeed wind tunnel
1965
2294
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0
Изотермические и неизотермические струи : Лекция : Для студентов-заочников специальности "Теплогазоснабжение и вентиляция"
1970
2780
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0
Use of single turning vane to eliminate flow separation in a space-limited 90° intake elbow of an axial-flow compressor
1965
1546
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Note on the time required for the achievement of steady flow past a slender body in a hypersonic shock tunnel
1961
769
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Some experiments with sonic throats downstream from the working-section of a slotted-wall high-speed tunnel
1957
2885
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Potential flow through cascades : A Comparison between exact and approximate solutions
1965
2992
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Wall interference in wind tunnels with slotted and porous boundaries at subsonic speeds
1954
1126
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Calibration of the flow in the working section of the 3ft×3ft tunnel, National aeronautical establishment
1956
1810
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An investigation of two methods of suppressing shock oscillation ahead of conical centre-body intakes
1962
866
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An exploratory investigation of skin friction and transition on three bodies of revolution at a Mach number of 1.61
1954
1470
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A flight investigation of the wake behind a meteor aircraft, with some theoretical analysis
1956
2391
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The response time of typical transducer - tube configuration for the measurement of pressures in high-speed wind tunnels
1966
1721
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Tests on probes designed to measure stagnation pressure directly in a supersonic stream
1974
2091
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