121–140 von 2,197 Ergebnissen
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    Data Summary from the First AIAA Computational Fluid Dynamics Drag Prediction Workshop

    David W. Levy / Thomas Zickuhr / John Vassberg et al. | AIAA | 2003
    Verlag: The American Institute of Aeronautics and Astronautics

    Boundary Layer Ingestion Benefit of the D8 Transport Aircraft

    Uranga, Alejandra / Drela, Mark / Greitzer, Edward M. et al. | AIAA | 2017
    transport aircraft, the D8 “double bubble,” carried out from 2010 to 2015 as part of a NASA ...
    Verlag: The American Institute of Aeronautics and Astronautics
    Schlagwörter: Commercial Aircraft , Aircraft Configurations

      Boundary Layer Ingestion Benefit of the D8 Transport Aircraft

      Uranga, Alejandra | Online Contents | 2017
      transport aircraft, the D8 “double bubble,” carried out from 2010 to 2015 as part of a NASA N+3 Phase 2 Program. A back-to-back comparison of non ...
      Verlag: AIAA , Reston, Va. [u.a.]

    NSU3D Results for the Second AIAA High-Lift Prediction Workshop

    Mavriplis, D. / Long, M. / Lake, T. et al. | British Library Conference Proceedings | 2015
    Verlag: American Institute of Aeronautics and Astronautics

    Constructal Design of Flying Wing Aircraft: Curved and Swept Configurations

    Izadpanahi, Ehsan / Rastkar, Siavash / Mardanpour, Pezhman | AIAA | 2019
    constructal law is a new concept that envisions the evolutionary design of aircraft. Nonlinear Aeroelastic Trim And Stability of HALE Aircraft ...
    Verlag: The American Institute of Aeronautics and Astronautics
    Schlagwörter: Model Aircraft , Aircraft Configurations

    Study of Droplet Shadow Zone of Aircraft Wing with Diffusion Effects

    Zhu, Cheng-Xiang / Tao, Ming-Jie / Zhao, Ning et al. | AIAA | 2019

    The aircraft deicing and detection tasks are complicated by the revealed existence of a shadow zone behind the wings, which contains no

     ...
    Verlag: The American Institute of Aeronautics and Astronautics
    Schlagwörter: Aircraft Wings , Ficks Law of Diffusion

    High-Fidelity Modeling of Multirotor Aerodynamic Interactions for Aircraft Design

    Alvarez, Eduardo J. / Ning, Andrew | AIAA | 2020

    Electric aircraft technology has enabled the use of multiple rotors in novel concepts for urban air mobility. However, multirotor

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

    AIAA Manuscript Review Process

    AIAA | 1997
    Verlag: The American Institute of Aeronautics and Astronautics

    Acoustics of Aircraft Engine-Duct Systems

    ALI H. NAYFEH / JOHN E. KAISER / AND DEMETRI P. TELIONIS | AIAA | 1975
    Verlag: The American Institute of Aeronautics and Astronautics

    Vertical Drop Test of Composite Fuselage Section of a Regional Aircraft

    Di Palma, L. / Di Caprio, F. / Chiariello, A. et al. | AIAA | 2019

    In this paper, a vertical drop test of a full composite fuselage section of a regional aircraft has been presented. This test was

     ...
    Verlag: The American Institute of Aeronautics and Astronautics
    Schlagwörter: Commercial Aircraft , Aircraft Structures

    Geometric Programming for Aircraft Design Optimization

    Hoburg, Warren / Abbeel, Pieter | AIAA | 2014

    Formulating conceptual-stage aircraft design problems as geometric programs, which are a specific type of convex optimization problem

     ...
    Verlag: The American Institute of Aeronautics and Astronautics
    Schlagwörter: Aircraft Design , Aircraft Systems , Aircraft Configurations

    Three-Way Spectral Decompositions of High-Performance Military Aircraft Noise

    Neilsen, Tracianne B. / Vaughn, Aaron B. / Gee, Kent L. et al. | AIAA | 2019
    three-way spectral decomposition quantifies the contribution from each noise type in the sound of a tied-down F-35B aircraft on a linear ground ...
    Verlag: The American Institute of Aeronautics and Astronautics
    Schlagwörter: High Performance Military Aircraft , Aircraft Engine Noise

    Source Localization of Crackle-Related Events in Military Aircraft Jet Noise

    Vaughn, Aaron B. / Gee, Kent L. / Swift, S. Hales et al. | AIAA | 2021
    apparent source locations of the steepest shocklike events in the noise field of a high-performance military jet aircraft using an event-based time ...
    Verlag: The American Institute of Aeronautics and Astronautics
    Schlagwörter: High Performance Military Aircraft , Jet Aircraft

    AIAA Manuscript Review Process

    AIAA | 1996
    Verlag: The American Institute of Aeronautics and Astronautics

    Global/Local Optimization of Aircraft Wing Using Parallel Processing

    Liu, Qiang / Jrad, Mohamed / Mulani, Sameer B. et al. | AIAA | 2016

    The structural optimization of a cantilever aircraft wing with stiffeners and curvilinear spars and ribs is described. The decomposition

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

      Global/Local Optimization of Aircraft Wing Using Parallel Processing

      Liu, Qiang | Online Contents | 2016
      Verlag: AIAA , Reston, Va. [u.a.]

      Global/Local Optimization of Aircraft Wing Using Parallel Processing

      Liu, Qiang | Online Contents | 2016
      The structural optimization of a cantilever aircraft wing with stiffeners and curvilinear spars and ribs is described. The decomposition ...
      Verlag: AIAA , Reston, Va. [u.a.]

    AIAA Manuscript Review Process

    AIAA | 1994
    Verlag: The American Institute of Aeronautics and Astronautics

    Aircraft Icing Severity Analysis Considering Three Uncertainty Types

    Feng, Kaixuan / Lu, Zhenzhou / Yun, Wanying | AIAA | 2018
    the icing severity index. In the process of predicting the aircraft icing severity grade, the membership function is introduced to describe ...
    Verlag: The American Institute of Aeronautics and Astronautics
    Schlagwörter: Aircraft Icing , Heat of Fusion

    Flight Performance with Respect to Rotor Rotation Directions of Multirotor Aircraft

    Kim, Hyeongseok / Lim, Daejin / Yee, Kwanjung | AIAA | 2023
    framework was developed to predict the flight performance of a general multirotor EVTOL aircraft. It was found that the FRRA concept minimizes ...
    Verlag: The American Institute of Aeronautics and Astronautics
    Schlagwörter: Aircraft Performance

    AIAA Manuscript Review Process

    AIAA | 1992
    Verlag: The American Institute of Aeronautics and Astronautics

    Noise characteristics of aircraft high lift systems

    Guo, Y.P. / Joshi, M.C. | Tema Archiv | 2003
    The characteristics of far-field noise from aircraft high lift systems are discussed. Analyses are made of the data from an airframe noise ...

    AIAA Manuscript Review Process

    AIAA | 1993
    Verlag: The American Institute of Aeronautics and Astronautics