In rotating machinery dynamics an orbit (Lissajous curve) represents the dynamic path of the shaft centerline motion during shaft rotation and resulting precession. The orbit can be observed with an oscilloscope connected to XY promixity probes. The orbits can also be simulated by a computer. The software for HP computer simulates orbits for two cases: (1) Symmetric orbit with four frequency components with different radial amplitudes and relative phase angles; and (2) Nonsymmetric orbit with two frequency components with two different vertical/horizontal amplitudes and two different relative phase angles. Each orbit carries a Keyphasor mark (one-per-turn reference). The frequencies, amplitudes, and phase angles, as well as number of time s...
Analytic platform inertial navigation system using single axis reference and pendulous integrating g...
Work performed at Catholic University on the research grant entitled Active Control of Robot Manipul...
In this paper, we analyze for stability the problem of planar vibrational motion of a satellite abou...
A mathematical model of a hingeless tilting rotor is presented. The model was obtained by a systemat...
A bibliography of papers and reports on geosynchronous orbits, as well as background papers concerne...
A capability was added to the general purpose finite element program NASTRAN Level 17.7 to conduct f...
This paper presents the Large Eddy Simulation (LES) of a propeller representative of the first roto...
LATDYN is a computer code for modeling the Large Angle Transient Dynamics of structures. The objecti...
A conceptual design of a visual system for a rotorcraft flight simulator is presented. Also, drive l...
Abstract Both sensors of the SEIS instrument (VBBs and SPs) are mounted on the mechanical leveling s...
An electro-mechanical analogue computer has been described which simulates in conjunction with the 1...
A star simulator is described which is capable of simulating a field of three or more stars in respo...
A simulator is described, which was designed for testing and evaluating inertial measuring units, an...
Des raies spectrales aux fréquences d'oscillation des pulsations qui les parcourent, la rotation des...
A computer program used to process the equations is presented, and a full description of equation im...
Analytic platform inertial navigation system using single axis reference and pendulous integrating g...
Work performed at Catholic University on the research grant entitled Active Control of Robot Manipul...
In this paper, we analyze for stability the problem of planar vibrational motion of a satellite abou...
A mathematical model of a hingeless tilting rotor is presented. The model was obtained by a systemat...
A bibliography of papers and reports on geosynchronous orbits, as well as background papers concerne...
A capability was added to the general purpose finite element program NASTRAN Level 17.7 to conduct f...
This paper presents the Large Eddy Simulation (LES) of a propeller representative of the first roto...
LATDYN is a computer code for modeling the Large Angle Transient Dynamics of structures. The objecti...
A conceptual design of a visual system for a rotorcraft flight simulator is presented. Also, drive l...
Abstract Both sensors of the SEIS instrument (VBBs and SPs) are mounted on the mechanical leveling s...
An electro-mechanical analogue computer has been described which simulates in conjunction with the 1...
A star simulator is described which is capable of simulating a field of three or more stars in respo...
A simulator is described, which was designed for testing and evaluating inertial measuring units, an...
Des raies spectrales aux fréquences d'oscillation des pulsations qui les parcourent, la rotation des...
A computer program used to process the equations is presented, and a full description of equation im...
Analytic platform inertial navigation system using single axis reference and pendulous integrating g...
Work performed at Catholic University on the research grant entitled Active Control of Robot Manipul...
In this paper, we analyze for stability the problem of planar vibrational motion of a satellite abou...