Sentence examples for maximize the thrust from inspiring English sources

The gradient-based numerical optimization model is used to maximize the thrust of solid rocket motor under a constraint of propellant weight.

While the principal purpose of the design of a rocket motor nozzle is to maximize the thrust, in thermal spraying, the main purpose is to obtain better coating quality.

A design optimization framework using an evolutionary algorithm and the Kriging surrogate model is developed and finds the optimum solution for multiple wing sails to maximize the thrust coefficient.

On the basis of the analytical field, the expressions of the flux linkage, back-electromotive force (EMF) and thrust force are acquired and examined, the chief design parameters, such as air gap length, pole number, magnet thickness and coil thickness, are optimized to maximize the thrust force of the MMSSM.

Gradient-based optimization is then used to locate the wing structure that maximizes the thrust, or minimizes the power under a thrust constraint, for a variety of shell boundary conditions.

And then to maximize the critical thrust force, the optimal design of an angle-ply laminate is performed to find the optimal number of fiber per millimeter, optimum diameter of fiber and optimum lamination angle using ADS Automated Design Synthesiss).

Moreover, it is a challenge to design large-scale SPPs that can maintain reliable fatigue strength and avoid vibration issues while maximizing the propeller thrust for a given power input.

To this end, we combine a three-dimensional version of the unsteady vortex lattice method (UVLM) with a deterministic global optimization algorithm to identify the optimal kinematics that maximize the propulsive efficiency under lift and thrust constraints.

Although a greater turn away from the stimulus results in lower performance, it would maximize the predator-prey distance, while a thrust enhancing, stage 2, counter-turn moves the heading of the fish back towards the initial stimulus.

Hashimoto and Ochiai [14, 15, 16] presented an entirely new optimum design methodology, in which the groove geometry can be flexibly changed by using the spline function, to maximize the stiffness of gas films for grooved thrust bearings.

The entire inlet system including the supersonic diffuser, throat, cowl lip, and subsonic diffuser sections was designed to maximize the total pressure recovery at the engine fan face to achieve maximum thrust by the engine at Mach 2.0 conditions.