Drag characteristics of a series of low-drag bodies of revolution at Mach numbers from 0.6 to 4.0
Drag characteristics of low drag bodies of revolution at Mach numbers from 0.6 to 4.0
DRAG↗
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Edge Disturbances in Axisymmetrical Shells of Revolution
Stress analysis of edge loaded, axisymmetric shells of revolution with Gaussian curvature - structural dynamics
BODY OF REVOLUTION↗
Scattering from bodies of revolution by point-matching
Point matching method application to acoustic scattering of plane waves from bodies of revolution
WAVE SCATTERING↗
Quasi-slender body theory for slowly oscillating bodies of revolution in supersonic flow
Quasi-slender body theory for slowly oscillating bodies of revolution in supersonic flow
SUPERSONIC FLOW↗
Transonic wind-tunnel measurements of some dynamic longitudinal and directional stability parameters for a finned spinning body of revolution having a high fineness ratio
Dynamic longitudinal and directional stability parameters for spinning body of revolution with high fineness ratio, at transonic speeds
DYNAMIC STABILITY↗
Heat-transfer and pressure distributions on a flat-face rounded-corner body of revolution with and without a flap at a Mach number of 8
Heat transfer and pressure distributions on flat face rounded-corner body of revolution with and without flap control at hypersonic speeds and angles of attack from 0 deg to 45 deg
FLAT SURFACE↗
On quasi-slender body theory for oscillating low aspect ratio wings and bodies of revolution in supersonic flow
Quasi-slender body theory for oscillating low aspect ratio wings and bodies of revolution in supersonic flow
LOW ASPECT RATIO WING↗
Analysis of the linearized supersonic flow about pointed bodies of revolution by the method of characteristics
Linearized supersonic flow about pointed bodies of revolution by method of characteristics
CHARACTERISTIC METHOD↗
The three-dimensional boundary layer on a body of revolution at small incidence and its stability.
Three-dimensional laminar boundary layer on body of revolution at small incidence at its stability
LAMINAR BOUNDARY LAYER↗
On heat transfer from isothermal and nonisothermal spinning bodies of revolution.
Forced convective heat transfer from isothermal and nonisothermal uniformly spinning bodies of revolution obtained by similar flow analysis
ROTATING BODY↗
Nonslender bodies of revolution having minimum pressure drag.
Nonslender bodies of revolution with minimum pressure drag, noting derivation of minimizing curves for Newtonian flow
SUPERSONIC FLOW↗
Axisymmetric thermal stresses in sandwich shells of revolution.
Reissner variational formulation of temperature distribution boundary value problem of axisymmetric thermal stresses in isotropic sandwich shells of revolution
TEMPERATURE DISTRIBUTION↗
Vibration and buckling of prestressed shells of revolution
Linearized set of equations developed for infinitesimal vibration and buckling of axisymmetrically prestressed thin shells of revolution
LINEAR EQUATION↗
On the state of membrane stress of shells of revolution with positive curvature
Integral stress function for state of membrane stress in shells of revolution formed by second- order surface
MEMBRANE FORCE↗
Study of the membrane stressed state of ellipsoidal shells of revolution with a regular row of holes
Membrane stresses in elliptical shells of revolution with several cuts
BODY OF REVOLUTION↗
On the criterion of dynamic stability of shallow shells of revolution
Dynamic stability of solid shallow shell of revolution with arbitrary elastic clamping at edge
DYNAMIC STABILITY↗
Stress concentration around a hole in an ellipsoidal shell of revolution
Equations for spherical shell used to determine stress state of shallow ellipsoidal shell of revolution weakened by hole
SHELL THEORY↗
Design of shells of revolution with a small hole at the apex under symmetrical and antisymmetrical load
Shells of revolution with small holes at apex, and determining stresses and moments under both symmetrical and asymmetrical loading
BENDING MOMENT↗