A METHOD FOR DETERMINING MODAL CHARACTERISTICS OF NONUNIFORM THIN CIRCULAR RINGS
Modes of nonuniform thin circular rings
RING↗
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RADIATIVE HEAT-TRANSFER CALCULATIONS FOR INFINITE SHELLS WITH CIRCULAR-ARC SECTIONS, INCLUDING EFFECTS OF AN EXTERNAL SOURCE FIELD
Diffuse radiation from infinite shells with circular-arc sections - source field effects
HEAT TRANSFER↗
Local Circumferential Buckling of Thin Circular Cylindrical Shells
The problem of circumferential buckling of a thin circular cylindrical shell due to compressive hoop stresses which vary in the axial direction is examined. For extremely localised compressive hoop stress distributions resulting from thermal discontinuity effects, or from a uniform, radial line loading, the buckle pattern should also be localised. Simplified analyses into these two types of problem are considered which show that only a limited number of buckle deflection modes needs to be assumed.
CYLINDRICAL SHELL↗
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↗
THE AERODYNAMIC CHARACTERISTICS OF A BODY IN THE FLOW FIELD NEAR THE TIP OF A CIRCULAR-ARC WING OF RECTANGULAR PLAN FORM AT A MACH NUMBER OF 2.01
Aerodynamic characteristics of body in flow field near tip of circular-arc wing of rectangular planform at mach 2.01
WING↗
STATIC LONGITUDINAL AND LATERAL STABILITY CHARACTERISTICS AT A MACH NUMBER OF 3.11 OF SQUARE AND CIRCULAR PLAN-FORM REENTRY VEHICLES, WITH SOME EFFECTS OF CONTROLS AND LEADING-EDGE EXTENSIONS
Static stability of square and circular planform reentry vehicles at mach 3.11 - effects of controls and leading-edge extensions
STATIC STABILITY↗
LARGE-SCALE WIND-TUNNEL TESTS OF A CIRCULAR PLAN-FORM AIRCRAFT WITH A PERIPHERAL JET FOR LIFT, THRUST, AND CONTROL
Wind tunnel tests of circular planform aircraft with peripheral jet for lift, thrust, and control
AIRCRAFT↗
An Experimental Investigation of Circular Internal-Compression Inlets with Translating Centerbodies Employing Boundary-Layer Removal at Mach Numbers from 0.85 to 3.50
Effect of boundary layer removal on total pressure recovery - circular internal compression inlets with translating centerbodies
INTERNAL COMPRESSION INLET↗
Vibration of Thin Circular Rings. Part II. Modal Functions and Eigenvalues of Constrained Semicircular Rings
The equations of motion of thin circular rings are derived and solved for in-plane in-extensional deformation. Modal characteristics are tabulated for the five lowest flexural modes of vibration of semicircular ring segments for the possible combinations of homogeneous boundary conditions that can occur.
RING↗
DRAG ON A RIGHT CIRCULAR CYLINDER IN RAREFIED FLOW AT LOW SPEED-RATIOS
Rarefied gas dynamics - drag coefficient of circular cylinder - characterization of fluid momentum exchange
DRAG COEFFICIENT↗
THE BUCKLING OF A FREE EDGE OF AN AXIALLY-COMPRESSED CIRCULAR CYLINDRICAL SHELL
Buckling of free edge of an axially-compressed circular cylindrical shell
CYLINDRICAL SHELL↗
BENDING VIBRATIONS OF A CIRCULAR CYLINDRICAL SHELL WITH AN INTERNAL LIQUID HAVING A FREE SURFACE
Resonant bending frequencies and mode shapes for thin circular cylindrical shell containing an internal liquid with a free surface
BENDING VIBRATION↗
LAUNCH WINDOW STUDIES EMPLOYING VARIATIONAL CALCULUS TO DETERMINE OPTIMUM THREE DIMENSIONAL TRAJECTORIES LEADING TO INJECTION INTO A SPACE-FIXED CIRCULAR ORBIT
Determination of optimum 3-dimensional trajectories to inject a saturn c-5 rocket into a space-fixed circular orbit
SPACECRAFT TRAJECTORY↗
A SET OF TWO-BODY ORBITAL PARAMETERS USEFUL FOR NEARLY CIRCULAR ORBITS AND SOME RELATED EQUATIONS
Description of a set of two-body orbital parameters useful for nearly circular orbits
ORBIT CALCULATION↗
OPTIMAL LOW-THRUST NEAR-CIRCULAR ORBITAL TRANSFER
Study of optimum low-thrust transfers between neighboring coplanar circular orbits for a simplified system model
ORBITAL TRANSFER↗
A LOOK AT MANNED ENTRY AT CIRCULAR TO HYPERBOLIC VELOCITIES
Manned space vehicle reentry at circular to hyperbolic velocities, considering deceleration, corridor width, heating, heat protection, vehicle weight, lateral ranging, and landing factors
REENTRY CONDITION↗
BENDING VIBRATIONS OF A CIRCULAR CYLINDRICAL SHELL WITH AN INTERNAL LIQUID HAVING A FREE SURFACE
Resonant bending frequencies and mode shapes for thin, circular cylindrical shell containing an internal liquid with a free surface
FUEL TANK↗
Comments on ''a note on the classical buckling load of circular cylindrical shells under axial compression''
Buckling load of circular cylindrical shells under axial compression
CYLINDRICAL SHELL↗