Results 1 to 10 of about 3,916 (88)

Investigation on Performance Characteristics of Hydrazine Monopropellant Thruster according to Reaction Chamber Adiabatic Temperature [PDF]

open access: yesفصلنامه علوم و فناوری فضایی, 2022
In this paper, by creating and developing a code based on thermodynamics and gas dynamics equations, the performance characteristics of a 1N hydrazine monopropellant thruster such as thrust force, specific impulse, characteristic exhaust velocity, and ...
Seyyed Rashad Rouholamini   +3 more
doaj   +1 more source

One-Way Wave Operator

open access: yesAcoustics, 2022
The second-order partial differential wave Equation (Cauchy’s first equation of motion), derived from Newton’s force equilibrium, describes a standing wave field consisting of two waves propagating in opposite directions, and is, therefore, a “two-way ...
Hans-Joachim Raida
doaj   +1 more source

Spherical One-Way Wave Equation

open access: yesAcoustics, 2021
The coordinate-free one-way wave equation is transferred in spherical coordinates. Therefore it is necessary to achieve consistency between gradient, divergence and Laplace operators and to establish, beside the conventional radial Nabla operator ∂Φ/∂r ...
Oskar Bschorr, Hans-Joachim Raida
doaj   +1 more source

Factorized One-Way Wave Equations

open access: yesAcoustics, 2021
The method used to factorize the longitudinal wave equation has been known for many decades. Using this knowledge, the classical 2nd-order partial differential Equation (PDE) established by Cauchy has been split into two 1st-order PDEs, in alignment with
Oskar Bschorr, Hans-Joachim Raida
doaj   +1 more source

Numerical investigation on jet characteristics and performance of SparkJet actuator based on pressure wave behavior inside a cavity

open access: yesAIP Advances, 2020
Thrust and total impulse performance of a SparkJet actuator are affected by pressure waves inside the cavity, so it is important to understand these effects.
Hyung-Jin Kim   +4 more
doaj   +1 more source

Effect of Spherical Silver Particles Size of the Catalyst Bed on Hydrogen Peroxide Monopropellant Thruster Performance [PDF]

open access: yesJournal of Applied Fluid Mechanics
In this paper, an analytical approach combined with a two-dimensional computational fluid dynamics (CFD) model is pursued to simulate the fluid flow in a monopropellant thruster for satellite propulsion systems.
F. Benzenine   +3 more
doaj   +1 more source

An analysis of Iran banking system balance sheet insolvency and its impact on economic growth using A DSGE model [PDF]

open access: yesسیاست‌گذاری اقتصادی
Purpose: Pricing The structure of Iranian financial systems is based on banking loans and credits. For this reason, Iranian commercial banks maintain the monopoly over supplying credits to various sectors.
Hasan Chenarani   +3 more
doaj   +1 more source

Performance Analysis of a Kerosene/Gaseous Oxygen Liquid Rocket Engine

open access: yesEngineering Proceedings
One of the most widely used rocket propulsion systems that uses liquid propellants is the liquid rocket engine. Due to their high density and specific impulse, liquid fuels and oxidizers are preferred.
Saravanan Ganesan   +4 more
doaj   +1 more source

A Nonlinear Damper with Dynamic Load and an Elastic Slit Membrane: Modeling and Interaction Analysis

open access: yesApplied Sciences
This article presents research into the feasibility of applying a nonlinear damper of a new conceptual structure. The key component of the damper is a circular membrane with slits that can move in a cylinder filled with viscous fluid.
Mostafa Sadeghian   +6 more
doaj   +1 more source

Thermodynamic performance modeling, optimization and numerical simulation of RBCC ejector mode

open access: yesPropulsion and Power Research
Ejector mode is a unique and critical phase of wide-range rocket-based combined cycle (RBCC) engine. In this paper, a quasi-one-dimensional thermodynamic performance modeling method, with more detailed model treatments for the inlet-diffuser system ...
Feiteng Luo   +5 more
doaj   +1 more source

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