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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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Computer program for finite difference solutions of linear asymmetric bending of elastic thin shell of revolution under arbitrary loading
Computer program on far field scattering pattern of arbitrary spherical wave by arbitrary surface of revolution
Analysis of elastic-plastic shells of revolution under axisymmetric loading by finite element method
Turbulent boundary layer characteristics of pointed slender bodies of revolution at supersonic speeds
Elastic shells of revolution axisymmetrically loaded analyzed, using multisegment method for solution of boundary value problems governed by nonlinear differential equations
Finite difference method stability analysis of deformed eccentrically stiffened shells of revolution, accounting for finite prebuckling rotations
Boundary value problem solution governed by system of partial differential equations applied to analysis of curved thin walled shells of revolution
Shells of revolution having arbitrary stiffness distribution of loads and temperatures
Reissner variational formulation of temperature distribution boundary value problem of axisymmetric thermal stresses in isotropic sandwich shells of revolution
Finite difference method stability analysis of deformed eccentrically stiffened shells of revolution, accounting for finite prebuckling rotations
Discussion concerning the calculation of the subsonic flow about unaligned thick bodies of revolution
Analysis of the common junction of three dissimilar general shells of revolution
Stress analysis of elastic-plastic shells of revolution containing discontinuities
Symmetrically loaded anisotropic shells of revolution
Dynamic and static stability of two blunt nosed low fineness ratio bodies of revolution in free flight - ballistics
High angle aerodynamic characteristics produced by nose cone of revolution in wind tunnel at supersonic speed
Digital computer program for geometrically nonlinear analysis of thin shells of revolution under axisymmetric loads
Aerodynamic coefficients and static stability characteristics of tangent ogive bodies of revolution - lift-to-drag, and fineness ratios