Flutter and divergence of rectangular wings of very low aspect ratio
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Fralich, Robert W↗
Engineering topics
Tuovila, W J
Publications and source records attributed to Tuovila, W J.
Experimentally Determined Natural Vibration Modes of Some Cantilever-wing Flutter Models by Using an Acceleration Method
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Hanson, Perry W↗
Aerodynamic damping at Mach numbers of 1.3 and 1.6 of a control surface on a two-dimensional wing by a free-oscillation method
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Tuovila, W J↗
Experimental flutter results for cantilever-wing models
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Tuovila, W J↗
Initial Experiments on Flutter of Unswept Cantilever Wings at Mach Number 1.3
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Tuovila, W J↗
Some flutter experiments at a Mach number of 1.3 on cantilever wings with tubular and closed bodies at the tips
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Mccarty, John Locke↗
Some wind-tunnel results of an investigation of the flutter of sweptback- and triangular-wing models at Mach number 1.3
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Tuovila, W J↗
Some experiments on the flutter of sweptback cantilever wing models at Mach number 1.3
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Tuovila, W J↗
Initial Experiments on Flutter of Unswept Cantilever Wings at Mach Number 1.3
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Tuovila, W J↗