1–20 von 596 Ergebnissen
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    Ablation Model Based on Porous Charring Layer Under Alumina Erosion Condition

    Liu, Yang / Li, Xiao-Cong / Li, Jiang et al. | AIAA | 2019
    model more complex. The chemical vapor deposition and thermal chemical ablation processes of pyrolysis gas and fuel gas in the porous structure ...
    Verlag: The American Institute of Aeronautics and Astronautics
    Schlagwörter: Chemical Vapor Deposition

    Ablation Predictions for Carbonaceous Materials Using Two Databases for Species Thermodynamics

    Milos, F. S. / Chen, Y.-K. | AIAA | 2013
    chemical equilibrium with applications model predicts a range of recession that is consistent with measurements for both heatshield cores. ...
    Verlag: The American Institute of Aeronautics and Astronautics
    Schlagwörter: Chemical Equilibrium

    Absolute rate constant measurements for the radiative combination ofatomic oxygen with nitric oxide

    HILL, K. D. / KINEYKO, W. R. | AIAA | 1971
    Verlag: The American Institute of Aeronautics and Astronautics

    Acoustic Response of Near-Equilibrium Diffusion Flames with Large Activation Energies

    Weiss, Adam D. / Sánchez, Antonio L. / Williams, Forman A. | AIAA | 2019

    The interaction of non-premixed flamelets with acoustic pressure waves of large characteristic wavelength, central to the development of

     ...
    Verlag: The American Institute of Aeronautics and Astronautics

    Acoustic Suppression in a Pulsed Chemical Laser

    Darrell R. Amherman / Irwin E. Alber / Eric Baum | AIAA | 1979
    Verlag: The American Institute of Aeronautics and Astronautics

    Active Subspace Variation and Modeling Uncertainty in a Supersonic Flame Simulation

    Wang, Nana / Yang, Tianwei / Ren, Zhuyin | AIAA | 2021
    chemical kinetics, turbulence combustion models, and boundary conditions, as well as to investigate the evolution of key physiochemical process ...
    Verlag: The American Institute of Aeronautics and Astronautics

    Advances in Computational Fluid Dynamics Methods for Hypersonic Flows

    Candler, Graham V. / Subbareddy, Pramod K. / Brock, Joseph M. | AIAA | 2014

    Over the past two decades or so, there have been many advances in the numerical simulation of hypersonic flows, with most effort focused

     ...
    Verlag: The American Institute of Aeronautics and Astronautics
    Schlagwörter: Chemical Energy

    Aerocapture Assessment for NASA Ice Giants Pre-Decadal Survey Mission Study

    Saikia, Sarag J. / Millane, James / Lu, Ye et al. | AIAA | 2021
    heat rate, total heat load, and the effect of postcapture orbit on the design parameters. Aerocapture mass benefit vs chemical capture is also ...
    Verlag: The American Institute of Aeronautics and Astronautics

    Aerodynamic Analysis of an Entry Capsule at Titan in Transition Regime

    Zuppardi, Gennaro / Mongelluzzo, Giuseppe | AIAA | 2022
    DS3V for the solution of three-dimensional flowfields. The Titan atmosphere is a mixture of nitrogen, methane, and argon. The chemical model is ...
    Verlag: The American Institute of Aeronautics and Astronautics

    Aerodynamic Design of Nozzles with Uniform Outflow for Hypervelocity Ground-Test Facilities

    Chan, Wilson Y. K. / Jacobs, Peter A. / Smart, Michael K. et al. | AIAA | 2018

    A method is proposed for the aerodynamic design of nozzles with uniform outflow for supersonic and hypersonic ground-test facilities

     ...
    Verlag: The American Institute of Aeronautics and Astronautics
    Schlagwörter: Chemical Equilibrium

    Aerothermodynamic Analysis of High-Altitude Space Launcher with Direct-Simulation Monte Carlo Method

    Cimini, M. / Pizzarelli, M. / Bernardini, M. | AIAA | 2019
    adopted numerical approach, a comparison of different air models is presented to highlight the effect of chemical reactions and molecules ...
    Verlag: The American Institute of Aeronautics and Astronautics

    Aerothermodynamics Behind a Blunt Body at Superorbital Speeds

    Park, Gisu / Gai, Sudhir L. / Neely, Andrew J. | AIAA | 2010
    Verlag: The American Institute of Aeronautics and Astronautics
    Schlagwörter: Chemical Equilibrium

    Afterburning Effects on Thermal Environment of Liquid Oxygen/Kerosene Rocket Under Low Altitudes

    Liang, Xiaoyang / Lu, Chenyu / Su, Yifei et al. | AIAA | 2022
    -ε turbulence model. Also, the nine-species and fourth-step chemical reactions are adopted to simulate ...
    Verlag: The American Institute of Aeronautics and Astronautics

    Aircraft Propulsion

    Roohi, Ehsan | AIAA | 2015
    Verlag: The American Institute of Aeronautics and Astronautics
    Schlagwörter: Chemical Rocket

    Aluminum Oxide–Supported Manganese Oxide Catalyst for a 98% Hydrogen Peroxide Thruster

    Surmacz, Pawel / Kostecki, Marek / Gut, Zbigniew et al. | AIAA | 2019
    the structure of the active phase. Test parameters and their change in time were analyzed. The influence of structural and chemical changes ...
    Verlag: The American Institute of Aeronautics and Astronautics

    A model of chemical releases leading to upper-atmospheric chemi-ion formation.

    FONTIJN, A. | AIAA | 1968
    Verlag: The American Institute of Aeronautics and Astronautics

    Analogy Between Vibrational and Chemical Nonequilibrium Effects on Stagnation Flows

    Luo, Jian / Wang, Zhi-Hui | AIAA | 2020

    The vibrational excitation and chemical reaction of diatomic molecules are two typical real gas effects that can significantly influence

     ...
    Verlag: The American Institute of Aeronautics and Astronautics
    Schlagwörter: Chemical Energy

    Analysis of a High-Efficiency Low-Emissions "Chemical Gas Turbine" System

    Takahisa Yamamoto / Tomohiko Furuhata / Norio Arai et al. | AIAA | 2002
    Verlag: The American Institute of Aeronautics and Astronautics

    Analysis of Energy Utilization for Chemical Rockets

    Riggins, David W. / Abbas, Mohammad / Wainwright, Mitchell et al. | AIAA | 2018

    Methodology is developed for the comprehensive analysis and quantification of energy utilization in chemical rockets, based on the

     ...
    Verlag: The American Institute of Aeronautics and Astronautics

    Analysis of Plume Infrared Signatures of S-Shaped Nozzle Configurations of Aerial Vehicle

    An, C. H. / Kang, D. W. / Baek, S. T. et al. | AIAA | 2016
    -dynamics code, the thermal flowfield and the distribution of chemical species within a plume, which are essential for the analysis of infrared ...
    Verlag: The American Institute of Aeronautics and Astronautics