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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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Elastoplastic analysis of circular cylindrical inclusion in uniformly stressed infinite homogeneous matrices of composite materials for aerospace applications
Critical buckling loads for circular cylindrical shells under axial compression
CDC 1604 computer program for circular lunar orbits for Gemini flights
Computer analysis of clamped circular plate response to axisymmetric impulsive load
Linearized wave equation with associated boundary conditions for predicting sound attenuation in soft walled circular ducts
Linear thermoelastic problems solved for thermal stress and displacement fields in elastic solids weakened by external circular cracks or plane of discontinuity
Probability distributions for errors in parameters of near-earth circular orbits with Apollo application
Computer methods for calculating particle trajectories and current collected by circular planar Langmuir probe mounted in satellite skin
Differential equations for natural frequencies of orthotropic circular plates of variable thickness
Bucking of thin-walled electroplated copper and Mylar circular cylinders under axial compression and bending
Analysis of launch windows from circular orbits for representative Mars missions
Transonic stator with multiple circular arc airfoils and minimum curvature tested over range of flow angles and velocities - stator A
Transonic stator with multiple circular arc airfoils and minimum curvature tested over range of flow angles and velocities - stator B
Transonic stator with double circular arc airfoils tested over range of flow angles and velocities
Reflection coefficient and admittance of circular aperture in ground plane covered by dielectric or plasma slab
Electrical impedance and radiation distributions of circular waveguide by integral transformation
Time function analysis for optimal control of satellite attitude and control jet fuel consumption in circular orbits
Solution for minimum fuel guidance from hyperbolic to circular orbit