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Institution

United Aircraft Corporation

CompanyMoscow, Russia
About: United Aircraft Corporation is a company organization based out in Moscow, Russia. It is known for research contribution in the topics: Propeller & Turbine. The organization has 3137 authors who have published 3410 publications receiving 38614 citations. The organization is also known as: UAC.


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Proceedings ArticleDOI

1,138 citations

Journal ArticleDOI
TL;DR: The well-known Whittaker-Kotel'nikov-Shannon sampling theorem for frequency-bandlimited functions of time is extended to functions of multidimensional arguments and it is shown that a function whose spectrum is restricted to a finite region of wave-number space may be reconstructed from its samples taken over a periodic lattice having suitably small repetition vectors.
Abstract: The well-known Whittaker-Kotel'nikov-Shannon sampling theorem for frequency-bandlimited functions of time is extended to functions of multidimensional arguments. It is shown that a function whose spectrum is restricted to a finite region of wave-number space may be reconstructed from its samples taken over a periodic lattice having suitably small repetition vectors. The most efficient lattice (i.e., requiring minimum sampling points per unit hypervolume) is not in general rectangular, nor is a unique reconstruction function associated with a given sampling lattice. The above results also apply to homogeneous wave-number-limited stochastic processes in the sense of a vanishing mean-square error. It is also found that, given a particular sampling lattice, the optimum (mean-square) presampling filter for nonwave-number-limited processes effects an ideal wave-number cutoff appropriate to the specified sampling lattice. Particular attention is paid to isotropic processes: minimum sampling lattices are specified up to eight-dimensional spaces, and a number of typical reconstruction functions are calculated.

648 citations

Journal ArticleDOI
TL;DR: In this article, a closed-form analytic solution for the optimum low thrust transfer between inclined circular orbits of different radii was found for the purpose of minimizing perturbations due to the atmosphere, the Earth's bulge, and the sun and moon.
Abstract: Propulsion requirements are determined for several controllable satellite missions. High thrust propulsion syslems such as chemical rockets and low thrust propulsion systems such as ion rockets are considered. Rendezvous missions are treated by determining minimum fuel maneuvers for small, simultaneous changes in the elements of quasi-circular orbits. Orbit transfer missions are treated by determining minimum fuel maneuvers for large changes in the elements of circular orbits. Orbit maintenance missions are treated by determining the propulsion necessary to cancel perturbations due to the atmosphere, the Earth's bulge, and the sun and moon. A closed-form analytic solution is found for the optimum low thrust transfer between inclined circular orbits of different radii. (auth)

289 citations

Journal ArticleDOI
TL;DR: Rotor wakes intrastator transport effects on high Mach number axial flow compressors performance, considering stagnation temperature profile and rotor blade loss factor, were investigated in this article, where they showed that rotor wake intrastation transport effects had a significant impact on axial Flow Compressor performance.
Abstract: Rotor wakes intrastator transport effects on high Mach number axial flow compressors performance, considering stagnation temperature profile and rotor blade loss factor

193 citations

Journal ArticleDOI
TL;DR: The CO2-peak of the i(E)-sweep curve (CO2peak) was observed in the case of CO2 on platinized platinum at 90°C.

187 citations


Authors

Showing all 3137 results

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Performance
Metrics
No. of papers from the Institution in previous years
YearPapers
20202
20143
20072
20062
20011
19981