THE BUCKLING OF A FREE EDGE OF AN AXIALLY-COMPRESSED CIRCULAR CYLINDRICAL SHELL
Buckling of a free edge of an axially compressed circular cylindrical shell
EDGE↗
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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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EFFECTS OF WING-CRANK, LEADING-EDGE CHORD EXTENSIONS AND HORIZONTAL-TAIL HEIGHT ON THE LONGITUDINAL STABILITY OF SWEPTWING MODELS AT MACH NUMBERS FROM 0.6 TO 1.4
Effects of wing-crank, leading-edge chord extensions & horizontal-tail height on longitudinal stability of swept-wing models
AERODYNAMIC STABILITY↗
WIND-TUNNEL TESTS OF THE STATIC LONGITUDINAL CHARACTERISTICS AT LOW SPEED OF A SWEPT-WING AIRPLANE WITH BLOWING FLAPS AND LEADING-EDGE SLATS
Low speed aerodynamic characteristics of swept- wing aircraft with blowing flaps and leading-edge slats
LEADING EDGE↗
AN ANALOG STUDY OF THE INFLUENCE OF INTERNAL MODIFICATIONS TO A WING LEADING EDGE ON ITS TRANSIENT TEMPERATURE RISE DURING HIGHSPEED FLIGHT
Aerodynamic heating of sweptback wing leading edge
SWEPTBACK WING↗
LARGE-SCALE WIND-TUNNEL TESTS IN GROUND EFFECT OF A 35 DEG SWEPTBACK WING JET TRANSPORT MODEL EQUIPPED WITH BLOWING BOUNDARY-LAYER-CONTROL TRAILING- AND LEADING-EDGE FLAPS
Wind tunnel test of ground effect of 35-deg swept- back wing jet transport equipped with boundary layer control, trailing & leading edge flaps
WIND TUNNEL STABILITY TEST↗
LEADING EDGE SLIP EFFECTS IN RAREFIED HYPERSONIC FLOW
Rarefied gas dynamics - sharp leading edge problem in rarefied hypersonic flow
HYPERSONIC FLOW↗
SHOCK STRUCTURE AND THE LEADING EDGE PROBLEM
Rarefied gas dynamics - low density flow near leading edge of flat plate in hypersonic stream
HYPERSONIC FLOW↗
EXPERIMENTAL STUDY OF HYPERSONIC RAREFIED FLOW NEAR THE LEADING EDGE OF A THIN FLAT PLATE
Rarefied gas dynamics - surface pressure & pitot pressure distribution in neighborhood of leading edge of thin flat plate
PRESSURE DISTRIBUTION↗
Some pressure-drag effects of rounding the leading edges of hypersonic inlets
Pressure-drag effects of rounding leading edges of hypersonic inlets
PRESSURE DRAG↗
Comparison of longitudinal aerodynamic characteristics of curved and straight lead- ing-edge delta wings at mach numbers 3 and 6
Longitudinal aerodynamic characteristics of delta wings with curved & straight leading edges from mach 3 to 6
DELTA WING↗
Some effects of control profile and control trailing-edge angle on the oscillating hinge-moment and flutter characteristics of flap-type controls at transonic speeds
Hinge moment and flutter characteristics of flap- type controls - free oscillation tests of changes in control profile and control trailing- edge angle
FLUTTER↗
Effect of edge loadings on the vibration of rectangular plates with various boundary conditions
Edge loading effect on vibration of rectangular plates with various boundary conditions
ORTHOTROPIC PLATE↗
Effects of leading-edge bluntness on pressure and heat-transfer measurements over a flat plate at a mach number of 20
Effects of leading edge bluntness on pressure and heat transfer at hypersonic speed
HEAT TRANSFER↗
Supersonic flutter of a thermally stressed flat panel with uniform edge loads
Supersonic flutter of thermally stressed flat panel with uniform edge loads
SUPERSONIC FLUTTER↗
Static aerodynamic characteristics of a rocket vehicle with thick wedge fins and sweptback leading and trailing edges
Static aerodynamic characteristics of rocket model vehicles with thick wedge fins with sweptback leading and trailing edges - supersonic wind tunnel testing of vehicle longitudinal stability
ROCKET VEHICLE↗
Edge Disturbances in Axisymmetrical Shells of Revolution
Stress analysis of edge loaded, axisymmetric shells of revolution with Gaussian curvature - structural dynamics
BODY OF REVOLUTION↗
Experimental investigation of thermal-buckling characteristics of flanged, thin-shell leading edges
Thermal buckling characteristics of flanged thin shell leading edges - aerodynamic heating
LEADING EDGE↗
Effects of leading-edge bluntness and ramp deflection angle on laminar boundary-layer separation in hypersonic flow
Leading edge bluntness and ramp deflection angle effects on laminar boundary layer separation in hypersonic flow
TWO-DIMENSIONAL FLOW↗