Stability Analysis of Elliptical Restricted Three Body Problem: Effects of Radiation and Triaxiality of Primaries in the Elliptical Restricted Three Body Problem - Softcover
Synopsis
The study here is for the equilibrium position of the primaries with the infinitesimal body. In particular, the possible positions of the equilibrium occurred when the three bodies form an equilateral triangle. The application of this model can be seen in the motion of Trojan - asteroids. The asteroids are only influenced by the gravitational forces of the Sun and Jupiter, and the orbit of Jupiter around Sun is assumed to be a fixed ellipse.
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Stability Analysis of Elliptical Restricted Three Body Problem
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Scholars' Press Apr 2020, 2020
ISBN 10: 6138928652
ISBN 13: 9786138928652
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Taschenbuch. Condition: Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -The study here is for the equilibrium position of the primaries with the infinitesimal body. In particular, the possible positions of the equilibrium occurred when the three bodies form an equilateral triangle. The application of this model can be seen in the motion of Trojan - asteroids. The asteroids are only influenced by the gravitational forces of the Sun and Jupiter, and the orbit of Jupiter around Sun is assumed to be a fixed ellipse. 184 pp. Englisch. Seller Inventory # 9786138928652
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Stability Analysis of Elliptical Restricted Three Body Problem
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Condition: New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. Autor/Autorin: Kumar Pandey KrishnaDr. Krishna Kumar pandey completed M.Sc( Mathematics) in the year 2006 from Govt. Science College Durg(C.G), India. He has Completed M.Phil in 2011 and Ph.D in July 2019 from Dr C.V. Raman University, Kota, Bila. Seller Inventory # 385853965
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Stability Analysis of Elliptical Restricted Three Body Problem: Effects of Radiation and Triaxiality of Primaries in the Elliptical Restricted Three Body Problem
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Stability Analysis of Elliptical Restricted Three Body Problem: Effects of Radiation and Triaxiality of Primaries in the Elliptical Restricted Three Body Problem
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Stability Analysis of Elliptical Restricted Three Body Problem | Effects of Radiation and Triaxiality of Primaries in the Elliptical Restricted Three Body Problem
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Taschenbuch. Condition: Neu. Stability Analysis of Elliptical Restricted Three Body Problem | Effects of Radiation and Triaxiality of Primaries in the Elliptical Restricted Three Body Problem | Krishna Kumar Pandey (u. a.) | Taschenbuch | 184 S. | Englisch | 2020 | Scholars' Press | EAN 9786138928652 | Verantwortliche Person für die EU: BoD - Books on Demand, In de Tarpen 42, 22848 Norderstedt, info[at]bod[dot]de | Anbieter: preigu. Seller Inventory # 118401588
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Stability Analysis of Elliptical Restricted Three Body Problem: Effects of Radiation and Triaxiality of Primaries in the Elliptical Restricted Three Body Problem
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Stability Analysis of Elliptical Restricted Three Body Problem
Published by
Scholars' Press Apr 2020, 2020
ISBN 10: 6138928652
ISBN 13: 9786138928652
New
Taschenbuch
Seller: buchversandmimpf2000, Emtmannsberg, BAYE, Germany
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Taschenbuch. Condition: Neu. This item is printed on demand - Print on Demand Titel. Neuware -The study here is for the equilibrium position of the primaries with the infinitesimal body. In particular, the possible positions of the equilibrium occurred when the three bodies form an equilateral triangle. The application of this model can be seen in the motion of Trojan - asteroids. The asteroids are only influenced by the gravitational forces of the Sun and Jupiter, and the orbit of Jupiter around Sun is assumed to be a fixed ellipse.VDM Verlag, Dudweiler Landstraße 99, 66123 Saarbrücken 184 pp. Englisch. Seller Inventory # 9786138928652
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Stability Analysis of Elliptical Restricted Three Body Problem : Effects of Radiation and Triaxiality of Primaries in the Elliptical Restricted Three Body Problem
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Taschenbuch. Condition: Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - The study here is for the equilibrium position of the primaries with the infinitesimal body. In particular, the possible positions of the equilibrium occurred when the three bodies form an equilateral triangle. The application of this model can be seen in the motion of Trojan - asteroids. The asteroids are only influenced by the gravitational forces of the Sun and Jupiter, and the orbit of Jupiter around Sun is assumed to be a fixed ellipse. Seller Inventory # 9786138928652