Synonyme wurden verwendet für: Wing flow flow
Suche ohne Synonyme: keywords:(Wing flow method tests)

41–60 von 248 Ergebnissen
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    Method of Calculating the Effect of a Gust on an Arbitrary Thin Wing

    S. M. Belotserkovskiy | NTIS | 1966
    Schlagwörter: Thin wing , Unsteady flow , Flow , Method , Wing

    Empirical Turbulence Interaction Noise Model for Permeable Flat Plate Leading Edges

    Geyer, Thomas F. / Enghardt, Lars | AIAA | 2024
    Schlagwörter: Aircraft Wing Design , Turbulent Flow , Wind Tunnel Tests

    Modulation and Annihilation of Aeroelastic Limit-Cycle Oscillations Using a Variable-Frequency Disturbance Generator

    Hughes, Michael T. / Gopalarathnam, Ashok / Bryant, Matthew | AIAA | 2023
    Schlagwörter: Wind Tunnel Tests , Flow Conditions , Aircraft Wing Design

    Towards Virtual Flight in Realistic Environments: A Hybrid Coupled Simulation Method

    Zholtovski, Stefan / Stephan, Anton / Holzäpfel, Frank | AIAA | 2020
    Schlagwörter: Wind Tunnel Tests , Incompressible Flow , Wing Geometry

    Low-Speed Wind-Tunnel Measurements of Surface Pressure Fluctuations on Two Slender-Wing Models

    D. A. Lovel / T. B. Owen | NTIS | 1971
    Schlagwörter: Conical flow , Wing flow method tests

    Investigation of the Unsteady Flow and Noise Generation in a Slat Cove

    Terracol, M. / Manoha, E. / Lemoine, B. | AIAA | 2015
    Schlagwörter: Flow Conditions , Wind Tunnel Tests , Lifting Wing

    Aircraft High-Lift Aerodynamic Analysis Using a Surface-Vorticity Solver

    E. D. Olson / C. W. Albertson | NTIS | 2016
    Schlagwörter: Potential flow , Wind tunnel tests , Wing span

    Multimodality in Aerodynamic Wing Design Optimization

    Bons, Nicolas P. / He, Xiaolong / Mader, Charles A. et al. | AIAA | 2019
    Schlagwörter: Blended Wing Body , Vortex Lattice Method , Flow Conditions

    Hybrid Wing Body Model Identification Using Forced-Oscillation Water Tunnel Data

    P. C. Murphy / D. D. Vicroy / B. Kramer et al. | NTIS | 2014
    Schlagwörter: Body-wing configurations , Water tunnel tests , Wind tunnel tests , Dynamic tests , Static tests , Flow visualization

    On the Use of Lifting Line Approaches for Propellers with Large Chord Variations

    Falissard, Fabrice / Pantel, Hugues | AIAA | 2024
    Schlagwörter: Aircraft Wing Design , Potential Flow , Fast Multipole Method

    Windtunnel Measurements on the Interference Between a Jet and a Wing Located Outside the Jet. Part 1: Text, Tables, and Figures

    Y. G. Kho | NTIS | 1979
    Schlagwörter: Peripheral jet flow , Wing profiles , Wind tunnel tests , Nozzle flow , Wing flaps

    Wind Tunnel Investigation of a Rigid Paraglider Reference Wing

    Belloc, H. | AIAA | 2015
    Schlagwörter: Wind Tunnel Tests , Wing Geometry , Flow Separation

    Comparison of Gradient-Based and Gradient-Enhanced Response-Surface-Based Optimizers

    Laurenceau, J. / Meaux, M. / Montagnac, M. et al. | AIAA | 2010
    Schlagwörter: Newton's Method , Transonic Flow , Wing Span

    Aeroelastic Characterization of a Flexible Wing Using Particle Tracking Velocimetry Measurements

    Mertens, Christoph / de Rojas Cordero, Tomás / Sodja, Jurij et al. | AIAA | 2021
    Schlagwörter: Rectangular Wing , Wind Tunnel Tests , Accelerating Flow

    Development of Reduced Unsteady Vortex Lattice Method Using Proper Orthogonal Decomposition Technique

    Cao, Bochao | AIAA | 2015
    Schlagwörter: Vortex Lattice Method , Rectangular Wing , Incompressible Flow

    Generation of Vortex Lift Through Reduction of Rotor/Stator Gap in Turbomachinery

    Du, Lin / Sun, Xiaofeng / Yang, Vigor | AIAA | 2015
    Schlagwörter: Incompressible Flow , Immersed Boundary Method , Flapping Wing

    Transient Growth Associated with Secondary Vortices in Ground/Vortex Interactions

    Stuart, Thomas A / Mao, Xuerui / Gan, Lian | AIAA | 2016
    Schlagwörter: Flow Patterns , Spectral Element Method , Wing Tip

    Applying Frequency-Domain Unsteady Lifting-Line Theory to Time-Domain Problems

    Bird, Hugh J. A. / Ramesh, Kiran | AIAA | 2021
    Schlagwörter: Vortex Lattice Method , Rectangular Wing , Incompressible Flow

    Wind Tunnel Testing of a 120th Scale Large Civil Tilt-Rotor Model in Airplane and Helicopter Modes

    C. R. Theodore / G. C. Willink / C. R. Russell et al. | NTIS | 2014
    Schlagwörter: Wind tunnel tests , Wing nacelle configurations , Flow visualization

    Effect of Small Surface Deformations on the Stability of Tollmien–Schlichting Disturbances

    Thomas, Christian / Mughal, Shahid M. / Roland, Hannah et al. | AIAA | 2018
    Schlagwörter: Natural Laminar Flow , Wing Geometry , Wind Tunnel Tests