Results 1 to 10 of about 413 (88)
Propulsion and launching analysis of variable-mass rockets by analytical methods
Propulsion and Power Research, 2013 In this study, applications of some analytical methods on nonlinear equation of the launching of a rocket with variable mass are investigated. Differential transformation method (DTM), homotopy perturbation method (HPM) and least square method (LSM) were
D.D. Ganji +4 more
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Simulation Model for Hardware-in-the-Loop Tests of the ILR-33 AMBER Rocket Control System [PDF]
SensorsIn this paper, an advanced flight simulation model of the ILR-33 AMBER rocket is shown. The model is designed for Hardware-in-the-Loop (HiL) tests of the rocket control system.
Dawid Cieśliński +4 more
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Heliyon, 2023 The geometry under consideration for this flow problem, namely paraboloid surface is similar to aircraft and car bonnet, bullet shape, front shape of submarine, rockets and these types of are useful in manufacturing of formula F1 cars and airplanes.
Muhammad Awais, T. Salahuddin
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Rotary Motion of Variable Mass Cylinder [PDF]
مجله مدل سازی در مهندسی, 2009 In this paper with the use of theory of variable mass systems and dynamic analysis, rotary motion of variable mass cylinder has been evaluated. Effects of angular rates, the methods of mass reduction and propellant burn, the shape and measurement of ...
سعدالدین +3 more
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Attitude Dynamics of a Spinning Rocket with Internal Fluid Whirling Motion [PDF]
INCAS Bulletin, 2014 This paper evaluates the impact that helical motion of fluid products of combustion within the combustion chamber of a rocket can have on the attitude dynamics of rocket systems.
Marius Ionut MARMUREANU, Ion FUIOREA
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Equations of motion for the variable mass flow-variable exhaust velocity rocket [PDF]
Astrodynamics Conference, 1972 An equation of motion for a one dimensional rocket is derived as a function of the mass flow rate into the acceleration chamber and the velocity distribution along the chamber, thereby including the transient flow changes in the chamber. The derivation of the mass density requires the introduction of the special time coordinate.
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General motion of a variable-mass flexible rocket with internal flow [PDF]
Journal of Spacecraft and Rockets, 1970 This paper consists of two parts. In the first part a new and general formulation of the dynamical problems associated with the powered flight of variable-mass , flexible rockets with internal gas flow is presented. The formulation comprises six ordinary differential equations for the rigid-body motion and three partial differential equations for the ...
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Shock and Vibration, 2011 Damping treatments have been extensively used as a powerful means to damp out structural resonant vibrations. Usually, damping materials are fully covered on the surface of plates.
Zheng Ling +3 more
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On the Angular Momentum of Rockets, Balloons, and Other Variable Mass Systems
, 2016 Variable mass systems are a classic example of open systems in classical mechanics. The reaction forces due to mass variation propel ships, balloons, and rockets. Unlike free constant mass systems, the angular momentum of these systems is not of constant magnitude due to the change in mass.
Nanjangud, Angadh, Eke, Fidelis
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Demonstration of dual-thrust capability in hybrid rockets using multi-layered tubular fuel grains
FirePhysChemThis study demonstrates the thrust modulation capabilities of a hybrid rocket motor employing a Multi-Layered Tubular (MLT) fuel grain. The MLT configuration involves arranging the fuel grains with distinct regression rates as layers.
Mengu Dinesh +2 more
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