1–19 von 19 Ergebnissen
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    Computational Fluid Dynamics Simulation of Hybrid Rockets of Different Scales

    Lazzarin, M. / Faenza, M. / Barato, F. et al. | AIAA | 2015
    Schlagwörter: Hybrid Rocket , Rocket Engine Performance , Antoine Equation

    Multiphysics Modeling for Combustion Instability in Paraffin-Fueled Hybrid Rocket Engines

    Casalino, Lorenzo / Ferrero, Andrea / Folcarelli, Lorenzo et al. | AIAA | 2024
    Schlagwörter: Hybrid Rocket Engines , Heat Equation

    Numerical Simulation of Ionized Rocket Plumes

    Gueyffier, D. / Fromentin-Denoziere, B. / Simon, J. et al. | AIAA | 2014
    Schlagwörter: Solid Rocket Motor , Rocket Performance , Maxwell Equation

    Liquid Films Instability Analysis of Liquefying Hybrid Rocket Fuels Under Supercritical Conditions

    Adachi, Masaki / Shimada, Toru | AIAA | 2014
    Schlagwörter: Hybrid Rocket Fuel , Redlich Kwong Equation of State , Hybrid Rocket Engines

    Validation of Transverse Instability Damping Computations for Rocket Engines

    Sattelmayer, Thomas / Kathan, Robert / Köglmeier, Stefan et al. | AIAA | 2015
    Schlagwörter: Rocket Engine , Liquid Rocket Combustion Chambers , Acoustic Wave Equation

    Small Satellite Rendezvous Using Differential Lift and Drag

    Horsley, M. / Nikolaev, S. / Pertica, A. | AIAA | 2013
    Schlagwörter: Rocket Engine , Clohessy Wiltshire Equation

    Algebraic Approach to the Minimum-Cost Multi-Impulse Orbit-Transfer Problem

    Avendaño, M. / Martín-Molina, V. / Martín-Morales, J. et al. | AIAA | 2016
    Schlagwörter: Tsiolkovsky Rocket Equation

    Rankine Vortex Formation in Cylindrical Tanks with Curved Base: An Experimental Investigation

    Harish, Sankar / Hariharan, S. K. / Shajahan, Ashiq et al. | AIAA | 2022
    Schlagwörter: Bernoulli's Equation , Liquid Propellant Rocket Engine

    Improved Linearized Breakup Model for the Liquid Sheets Produced by Swirl Atomizers

    Arun Vijay, G. / Shenbaga Vinayaga Moorthi, N. | AIAA | 2015
    Schlagwörter: Liquid Fuel Rocket , Continuity Equation

    Linear Acoustic Analysis of Main Combustion Chamber of an Oxidizer-Rich Staged Combustion Engine

    Lioi, Christopher / Ku, David / Yang, Vigor | AIAA | 2018
    Schlagwörter: Acoustic Wave Equation , Liquid Rocket Engine

    Theoretical and Experimental Investigations on the Acoustic Absorptions of Baffled Injectors

    Zhu, Shuoshuo / Li, Jingxuan / Liu, Wang et al. | AIAA | 2021
    Schlagwörter: Acoustic Wave Equation , Liquid Rocket Engine

    Review of "Computation of Viscous Incompressible Flows"

    Kaltayev, Aidarkhan | AIAA | 2012
    Schlagwörter: Poisson's Equation , Liquid Propellant Rocket Engine

    Performance Scalability of Square Solar Sails

    Trofimov, Sergey P. / Ovchinnikov, Mikhail Yu. | AIAA | 2017
    Schlagwörter: Tsiolkovsky Rocket Equation

    Stability Index for Injection-Coupled Instability in Full-Scale Firing Tests

    Kobayashi, Kan / Nunome, Yoshio / Tomita, Takeo et al. | AIAA | 2017
    Schlagwörter: Acoustic Wave Equation , Rocket Combustor

    Parameterizing the Search Space of Starshade Fuel Costs for Optimal Observation Schedules

    Soto, Gabriel J. / Savransky, Dmitry / Garrett, Daniel et al. | AIAA | 2019
    Schlagwörter: Tsiolkovsky Rocket Equation

    Numerical Strategy for Unsteady Two-Way Coupled Polydisperse Sprays: Application to Solid-Rocket Instabilities

    Doisneau, F. / Sibra, A. / Dupays, J. et al. | AIAA | 2014
    Schlagwörter: Solid Rocket Motor , Williams Boltzmann Equation

    Compressible Model for Dilute Flows

    Petitpas, Fabien / Daniel, Eric | AIAA | 2014
    Schlagwörter: Williams Boltzmann Equation , Solid Rocket Motor

    Injector Head Transpiration Cooling Coupled with Combustion in H 2 / O 2 Subscale Thrust Chamber

    Zhu, Yinhai / Jiang, Peixue / Sun, Jiguo et al. | AIAA | 2012
    Schlagwörter: Equation of States , Rocket Thrust Chamber

    Analysis of a Cylindrical Specimen Heated by an Impinging Hot Hydrogen Jet

    Wang, Ten-See / Luong, Van / Foote, John et al. | AIAA | 2010
    Schlagwörter: Nuclear Engine for Rocket Vehicle Application , Conduction Equation