Add to ORKGThe effect of Mach number and structural damping on single-degree-of-freedom pitching of a wing is presented. Some experimental results are compared with theory and good agreement is found for certain ranges of an inertia parameter
Design for prevention of aeroelastic instability (that is, the critical speeds leading to aeroelasti...
The effects on flutter of the aerodynamic interaction between the space shuttle bodies and wing, 1/8...
Several very low aspect ratio flat plate wing configurations are analyzed for their aerodynamic inst...
The effect of Mach number and structural damping on single-degree-of-freedom pitching of a wing is p...
Part I describes vibration tests, in a wind tunnel, of simple airfoils and of the tail plane of an M...
The results of some wind-tunnel experiments to investigate the effects of aspect ratio and Mach numb...
Results of four thin, unswept, flutter airfoils attached to two freely falling bodies are reported. ...
A number of calculations of bending-torsion wing flutter are made at two Mach numbers, m=0 (incompre...
This report presents a survey of previous theoretical and experimental investigations on wing flutte...
A method is presented for the calculation of the flutter speed of a uniform wing carrying an arbitra...
The flow-field characteristics beneath swept and unswept wings as determined by potential-flow theor...
The present paper is a continuation of the general study of flutter published in NACA reports nos. 4...
This report gives the results of a detailed study of the flutter characteristics of four representat...
The results of the basic flutter theory originally devised in 1934 and published as NACA Technical R...
Transonic flutter and buffet results obtained from wind-tunnel tests of a low aspect ratio semispan ...
Design for prevention of aeroelastic instability (that is, the critical speeds leading to aeroelasti...
The effects on flutter of the aerodynamic interaction between the space shuttle bodies and wing, 1/8...
Several very low aspect ratio flat plate wing configurations are analyzed for their aerodynamic inst...
The effect of Mach number and structural damping on single-degree-of-freedom pitching of a wing is p...
Part I describes vibration tests, in a wind tunnel, of simple airfoils and of the tail plane of an M...
The results of some wind-tunnel experiments to investigate the effects of aspect ratio and Mach numb...
Results of four thin, unswept, flutter airfoils attached to two freely falling bodies are reported. ...
A number of calculations of bending-torsion wing flutter are made at two Mach numbers, m=0 (incompre...
This report presents a survey of previous theoretical and experimental investigations on wing flutte...
A method is presented for the calculation of the flutter speed of a uniform wing carrying an arbitra...
The flow-field characteristics beneath swept and unswept wings as determined by potential-flow theor...
The present paper is a continuation of the general study of flutter published in NACA reports nos. 4...
This report gives the results of a detailed study of the flutter characteristics of four representat...
The results of the basic flutter theory originally devised in 1934 and published as NACA Technical R...
Transonic flutter and buffet results obtained from wind-tunnel tests of a low aspect ratio semispan ...
Design for prevention of aeroelastic instability (that is, the critical speeds leading to aeroelasti...
The effects on flutter of the aerodynamic interaction between the space shuttle bodies and wing, 1/8...
Several very low aspect ratio flat plate wing configurations are analyzed for their aerodynamic inst...