Synonyme wurden verwendet für: Aircraft
Suche ohne Synonyme: title: AIAA Journal of Aircraft

121–140 von 2,211 Ergebnissen
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    Inverse Design Method for Low-Boom Supersonic Transport with Lift Constraint

    Ding, Yu-Lin / Han, Zhong-Hua / Qiao, Jian-Ling et al. | AIAA | 2023

    The low-boom inverse design method is of great interest for the preliminary design of supersonic transport (SST), owing to its good

     ...
    Verlag: The American Institute of Aeronautics and Astronautics
    Schlagwörter: Aircraft Components and Structure , Aircraft Wing Design

    Simulating Airplane Aerodynamics with Body Forces: Actuator Line Method for Nonplanar Wings

    Kleine, Vitor G. / Hanifi, Ardeshir / Henningson, Dan S. | AIAA | 2023

    Two configurations typical of fixed-wing aircraft are simulated with the actuator line method (ALM): a wing with winglets, and a T tail

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    Verlag: The American Institute of Aeronautics and Astronautics
    Schlagwörter: Aircraft Components and Structure , Fixed Wing Aircraft

    Numerical Study on Wind-Driven Thin Water Film Runback on an Airfoil

    Chen, Ningli / Yi, Xian / Wang, Qiang et al. | AIAA | 2023
    transportation of a wind-driven thin film caused by the impingement of water droplets. The external flow of air and droplets is simulated using the EMF ...
    Verlag: The American Institute of Aeronautics and Astronautics
    Schlagwörter: Aircraft Icing

    Fluidic-Oscillator-Based Pulsed Jet Actuation on a Vertical Tail

    Löffler, Stephan / Weiss, Julien | AIAA | 2023
    different active flow control (AFC) settings, rudder deflection, and sideslip angles at a chord Reynolds number of 1.3 million. In addition to ...
    Verlag: The American Institute of Aeronautics and Astronautics
    Schlagwörter: Aircraft Design , Aircraft Stability and Control

    Performance, Aerodynamics, and Aeroacoustics of Side-by-Side Rotors Using High-Fidelity Computational Fluid Dynamics

    Sagaga, Jared / Lee, Seongkyu | AIAA | 2023

    This paper investigates the performance, aerodynamics, and aeroacoustics of NASA’s side-by-side urban air mobility (UAM) aircraft in

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    Verlag: The American Institute of Aeronautics and Astronautics

    Novel High-Precision and Efficient Momentum Source Method

    Cao, Tianshi / Bai, Junqiang / Feng, Shaodong et al. | AIAA | 2023
    method (SMM), with a maximum error of 5% in aircraft lift and drag coefficients compared with experimental values. Meanwhile, the calculation ...
    Verlag: The American Institute of Aeronautics and Astronautics
    Schlagwörter: Civil Aircraft , Aircraft Design Process

    Improved Dynamic Geometry Control Algorithms for Efficient Aerodynamic Shape Optimization

    Streuber, Gregg M. / Zingg, David W | AIAA | 2023
    performance tradeoffs at various stages of optimization, enforcing arbitrary constraints on open-ended optimization, and necessitating foreknowledge ...
    Verlag: The American Institute of Aeronautics and Astronautics
    Schlagwörter: Aircraft Components and Structure , Aircraft Design

    Pulsed Velocity Created by a Plasma Actuator in the Vicinity of the Wall

    Zhang, Xin / Huang, Yong | AIAA | 2023
    attracted worldwide attention for aircraft flow control in the last two decades. It is believed that understanding the flowfield generated by ...
    Verlag: The American Institute of Aeronautics and Astronautics

    Force/Moment-Conserving Pressure Mapping Scheme for Fluid/Structure Interaction Analysis

    Beom Lee, Kyu / Yeon Cho, Jin / Ho Kim, Jeong | AIAA | 2023
    for FSI analysis. However, for most existing mapping algorithms, the sum of force/moment, which is one of the most important physical ...
    Verlag: The American Institute of Aeronautics and Astronautics
    Schlagwörter: Multidisciplinary Aircraft Design

    Assessment of Compressibility Corrections on Spalart–Allmaras Turbulence Model for High-Mach-Number Flows

    Xue, Yunlong / Feng, Yongliang / Zheng, Xiaojing | AIAA | 2023
    Validation of the Spalart–Allmaras Turbulence Model in Parallel Environment,” Journal of Aircraft, Vol. 42, No. 1, 2005, pp. 179–188 ...
    Verlag: The American Institute of Aeronautics and Astronautics

    Flow Topology of a Slanted Cylinder with Rounded-Edges Under Compressible Conditions

    Huss, Rhylan A. / Zigunov, Fernando / Alvi, Farrukh | AIAA | 2023

    In this study, the slanted afterbody was modified to more closely represent cargo aircraft afterbodies through the addition of a basal

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    Verlag: The American Institute of Aeronautics and Astronautics

    Deep-Learning Strategy Based on Convolutional Neural Network for Wall Heat Flux Prediction

    Dai, Gang / Zhao, Wenwen / Yao, Shaobo et al. | AIAA | 2023

    Aerodynamic thermal prediction plays an important role in the design of hypersonic aircraft, especially in the design of the aircraft’s

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    Verlag: The American Institute of Aeronautics and Astronautics
    Schlagwörter: Hypersonic Aircraft

    Duct Effects on Acoustic Source Radiation

    Baddour, Benjamin / Joseph, Phillip / McAlpine, Alan et al. | AIAA | 2023

    This paper presents a detailed numerical investigation of the effects of a semi-infinite hard-walled duct on the radiation due to point

     ...
    Verlag: The American Institute of Aeronautics and Astronautics
    Schlagwörter: Aircraft Engines

    Vortex Identification and Quantification on Blunt Trailing-Edge Rotor Blades in Reverse Flow

    Wild, Oliver D. / Jones, Anya R. | AIAA | 2023

    An inherent aerodynamic limitation of high-advance-ratio high-speed helicopters is reverse flow on the retreating blades, which can be a

     ...
    Verlag: The American Institute of Aeronautics and Astronautics
    Schlagwörter: Aircraft Wing Design

    Spatial Transformations for Reacting Gas Shock Tube Experiments

    Clarke, Justin / Di Mare, Luca / McGilvray, Matthew | AIAA | 2023
    in a shock tube contains many flow nonuniformities, in particular boundary-layer effects. For the purpose of studying the properties of the ...
    Verlag: The American Institute of Aeronautics and Astronautics
    Schlagwörter: Aircraft Operations , Equations of Fluid Dynamics

    FFVHC-ACE: Fully Automated Cartesian-Grid-Based Solver for Compressible Large-Eddy Simulation

    Asada, Hiroyuki / Tamaki, Yoshiharu / Takaki, Ryoji et al. | AIAA | 2023
    ., Journal of Aircraft, Vol. 56, No. 2, 2019, pp. 621–644). Furthermore, the wall-modeled LES at the real-flight Reynolds number shows good ...
    Verlag: The American Institute of Aeronautics and Astronautics

    Equivalent Area Targets for Inverse Design Optimization With Changing Low-Boom Cruise Conditions

    Wu Li | NTRS | 2023
    ) of low-boom supersonic aircraft when the cruise condition changes during the optimization iterations. A modified linear theory for steady ...
    Verlag: American Institute of Aeronautics and Astronautics
    Schlagwörter: scaling of optimal target , invariance of optimal targets

    Three-Dimensional Quantitative Flow Visualization Around a Thrust Reverser

    Hysa, Ilda / Tuinstra, Marthijn / Sciacchitano, Andrea et al. | AIAA | 2023
    aircraft model with jet engines operating with thrust reversers. The engine jet and freestream flow velocity are varied to yield a jet to ...
    Verlag: The American Institute of Aeronautics and Astronautics
    Schlagwörter: Aircraft Components and Structure

    Copula-Based Collaborative Multistructure Damage Diagnosis and Prognosis for Fleet Maintenance Digital Twins

    Zhou, Xuan / Sbarufatti, Claudio / Giglio, Marco et al. | AIAA | 2023
    Verlag: The American Institute of Aeronautics and Astronautics
    Schlagwörter: Aircraft Components and Structure , Number of Particles

    Complex Standard Eigenvalue Problem Derivative Computation for Laminar–Turbulent Transition Prediction

    Shi, Yayun / Song, Chao / Chen, Yifu et al. | AIAA | 2023
    method is widely used in engineering applications and is the preferred method for laminar flow optimization. However, the further development of ...
    Verlag: The American Institute of Aeronautics and Astronautics
    Schlagwörter: Aircraft Wing Design