A matrix method for calculating the source function, mean intensity, and flux in a model atmosphere
Matrix method for calculating source function, mean intensity, and flux in model stellar atmosphere
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Matrix method for calculating source function, mean intensity, and flux in model stellar atmosphere
Mathematical models for determining eigenvalue bounds of matrix
Mathematical model for beam and plate vibration in bending modes using lumped parameters
Linear optimal control technique for flexible- booster control system design, showing drift minimum model with matrix transformations for closed-loop dynamics
Designing lightweight, robust cryogenic storage tanks is critical for future launch vehicles, in-space propellant storage, and hydrogen powered aircraft. This work presents a multiscale modeling and Bayesian optimization framework for the design of thermoplastic matrix composite cryotanks. Molecular dynamics simulations are first used to determine temperature-dependent constituent properties for candidate thermoplastic matrices, which are homogenized to the lamina scale using NASA’s Multiscale Analysis Tool (NASMAT). These lamina properties, in combination with laminate family generation rules, are evaluated in HyperX structural optimization software to identify stacking sequences that meet all cryogenic load requirements. A Bayesian optimization framework is applied, with HyperX in the loop (via the HyperX API) to efficiently search across material and laminate design variables, yielding an optimized cryotank configuration with significant reductions in design cycle time compared to exhaustive search approaches.
Model atmosphere source function, mean intensity and flux by matrix methods
Nilsson model used to derive expressions for nuclear matrix elements, considering forbidden beta decay of spheroidal-shaped nuclei
Semiatomistic model for nonductile fracture based on analysis of static and dynamic stress concentrations in uniaxial fiber-matrix composite materials
Deployment dynamics analysis of large surface in orbit and on test stand
Boundary condition constraint method for generalizing R-matrix theory, permitting use of shell model as basis for nuclear-reaction calculations
Recursive algorithm for identification of time varying parameters of system, noting use for matrix inversion
Geometric interpretation of product form of inverse applied to sparse matrices in linear programming, using graph theory
Book on analytical methods in vibrations covering general mathematical formulations of common features of various vibrating systems
Integrated program management process provides management visual assistance through three interrelated charts - system model that identifies each function to be performed, matrix that identifies personnel responsibilities for these functions, process chart that breaks down the functions into discrete tasks.
Matrix-Holzer method for predicting free vibration modes of clustered launch vehicles in bending applied to first eight modes of Saturn I model
Matrix-Holzer method for predicting free vibration modes of clustered launch vehicles in bending applied to first eight modes of Saturn I model
Mathematical theory of dimensional analysis and similitude, application to spacecraft thermal design and experimental results
Minimum realization of linear time-varying nonanticipative system characterized by its impulse response matrix