FLUTTER TESTS OF SANDWICH-TYPE FLAT PANELS AT MACH NUMBERS OF 2.97 AND 4.12
Flutter tests of sandwich-type flat panels at supersonic speeds
FLUTTER↗
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SOME EFFECTS OF VARIATIONS IN DENSITY AND AERODYNAMIC PARAMETERS ON THE CALCULATED FLUTTER CHARACTERISTICS OF FINITE-SPAN SWEPT AND UNSWEPT WINGS AT SUBSONIC AND SUPERSONIC SPEEDS
Subsonic and supersonic flutter calculations on swept and unswept wings to evaluate effects of variations in aerodynamic parameters and density
FLOW CHARACTERISTICS↗
EXPERIMENTAL AND CALCULATED RESULTS OF A FLUTTER INVESTIGATION OF SOME VERY LOW ASPECT-RATIO FLAT-PLATE SURFACES AT MACH NUMBERS FROM 0.62 TO 3.00
Flutter investigation of very low aspect-ratio flat-plate surfaces at subsonic and supersonic speed
ALUMINUM ALLOY↗
FREE-FLIGHT TESTS OF 45 DEG SWEPT WINGS OF ASPECT RATIO 3.15 AND TAPER RATIO 0.54 TO MEASURE WING DAMPING OF THE FIRST BENDING MODE AND TO INVESTIGATE THE POSSIBILITY OF FLUTTER AT TRANSONIC SPEEDS
Free flight tests of 45-deg swept wings of 3.15 aspect ratio and 0.54 taper ratio to measure wing damping and possible transonic flutter
FLUTTER↗
ANALYSIS OF THE FLUTTER OF FLAT RECTANGULAR PANELS ON THE BASIS OF EXACT THREE-DIMENSIONAL LINEARIZED SUPERSONIC POTENTIAL FLOW
Analysis of flutter of flat rectangular panels at low supersonic mach numbers using air forces from exact linearized potential-flow theory
FLUTTER↗
FLUTTER ANALYSIS OF FLAT RECTANGULAR PANELS BASED ON THREE-DIMENSIONAL SUPERSONIC POTENTIAL FLOW
Analysis of flutter of flat rectangular panels at low supersonic mach numbers using air forces from exact linearized potential-flow theory
FLUTTER↗
Comparative evaluation of methods for predicting flutter and divergence of unswept wings of finite span
Predicting flutter and divergence of unswept wings at subsonic & supersonic speeds
SUBSONIC FLUTTER↗
Experimental and calculated supersonic flutter characteristics of models of the x-15 horizontal and vertical tails
Experimental and calculated supersonic flutter characteristics of X-15 horizontal and vertical tails
TAIL SURFACE↗
Flutter investigation of streamwise-oriented arrays of curved panels under compressive loading and aerodynamic heating
Flutter characteristics tested on cylindrical segments of longitudinal arrays of rectangular curved panels under compressive loading and aerodynamic heating
COMPRESSION LOADING↗
Flutter of a simply supported panel subjected to a nonlinear temperature distribution and supersonic flow.
Parabolic temperature distribution effect on flutter behavior of panel subjected to supersonic flow over one surface
TEMPERATURE DISTRIBUTION↗
The role of boundary conditions on flutter of orthotropic panels.
Flutter of rectangular orthotropic panel supported by deflectional spring along two edges in supersonic airflow
PANEL FLUTTER↗
Supersonic Flutter of a Cylindrical Shell with Application to the Centaur Interstage Adapter
Analytic solution to flutter boundaries of circular cylindrical shell subjected to supersonic flow with application to Centaur interstage adapter
CENTAUR LAUNCH VEHICLE↗
Supersonic flutter of flat rectangular orthtropic panels elastically restrained against edge rotation
Supersonic flutter analysis for flat loaded orthotropic panels with edge restraint
FLUTTER ANALYSIS↗
Transonic flutter investigation of models of proposed horizontal tails for the X-15 airplane
Transonic flutter analysis of dynamically and elastically scaled models of all-movable horizontal tail of X-15 aircraft
TRANSONIC FLUTTER↗
Transonic flutter investigation of models of the X-15 airplane horizontal tail
Transonic flutter analysis of dynamically and elastically scaled models of sweptback, tapered, all-movable horizontal tail of X-15 aircraft
SCALE MODEL↗
Effects of modifications to a control surface on a 6-percent-thick unswept wing on the transonic control-surface flutter derivatives
Transonic flutter derivatives for unswept wing control surface configurations determined by pressure cell measurements
UNSWEPT WING↗
Transonic flutter investigation of models of a proposed variable-sweep wing
Transonic flutter analysis of variable sweep wing models
VARIABLE SWEEP↗
User's manual for a Fortran IV program for computing flutter boundaries of flat panel arrays in supersonic flow
Fortran IV program manual for computing flutter boundaries of flat panel arrays in supersonic flow
PANEL FLUTTER↗