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

1–20 von 253 Ergebnissen
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    Parameterized aeroelastic modeling and flutter analysis for a folding wing

    Zhao, Yonghui / Hu, Haiyan | Tema Archiv | 2012
    Schlagwörter: Tragflügelumströmung , DLM (doublet lattice method)

    Numerical simulation and wind tunnel tests investigation and validation of a morphing wing-tip demonstrator aerodynamic performance

    Şugar Gabor, Oliviu / Koreanschi, Andreea / Botez, Ruxandra Mihaela et al. | Elsevier | 2016
    Schlagwörter: Morphing wing , Infra-red tests , Wind tunnel tests , Laminar-to-turbulent flow transition

    Dynamic Stall Suppression Using Combustion-Powered Actuation (COMPACT)

    C. G. Matalanis / P. O. Bowles / S. Jee et al. | NTIS | 2016
    Schlagwörter: Wind tunnel tests , Rotary wing aircraft , Flow distribution , Two dimensional flow , Wing span , Wing slots , Three dimensional flow

    Morphing wing optimization for steady level flight

    Körpe, Durmuş S / Özgen, Serkan | SAGE Publications | 2017
    Schlagwörter: panel method , boundary layer flow , Morphing wing

    Two-Dimensional Low-Speed Tunnel Tests on the Naca 0012 Section Including Measurements Made During Pitching Oscillations at the Stall

    G. F. Moss / P. M. Murdin | NTIS | 1971
    Schlagwörter: Wing oscillations , Wing profiles , Two dimensional flow , Wind tunnel stability tests , Wing flow method tests

    Vortex-Sheet Representation of Leading-Edge Vortex Shedding from Finite Wings

    Hirato, Yoshikazu / Shen, Minao / Gopalarathnam, Ashok et al. | AIAA | 2019
    Schlagwörter: Rectangular Wing , Vortex Lattice Method , Wing Root , Two Dimensional Flow , Flow Separation

    The Behaviour of the Leading-Edge Vortices over a delta Wing Following a Sudden Change of Incidence

    D. W. Bryer / N. C. Lambourne / J. F. Maybrey | NTIS | 1970
    Schlagwörter: Flow visualization , Cross flow , Wing flow method tests , Wing loading

    Assessment of body-freedom flutter for an unmanned aerial vehicle

    Schäfer, D. / Vidy, C. / Mack, C. et al. | Online Contents | 2018
    Schlagwörter: Euler method , Potential flow theory , Flying wing combat UAV

    Invariant Formulation for the Minimum Induced Drag Conditions of Nonplanar Wing Systems

    Demasi, Luciano / Dipace, Antonio / Monegato, Giovanni et al. | AIAA | 2014
    Schlagwörter: Potential Flow , Wing Tip , Vortex Lattice Method , Wing Geometry

    Effect of Wing Flexibility on the Experimental Aerodynamic Characteristics of an Oblique Wing

    E. J. Hopkins / S. C. Yee | NTIS | 1977
    Schlagwörter: Wing flow method tests , Wing loading

    Comparison of Wind Tunnel Test Results at Free Stream Mach 0.7 with Results from the Boeing Tea-230 Subsonic Flow Method

    L. W. Mohn | NTIS | 1975
    Schlagwörter: Potential flow , Subsonic flow , Wind tunnel stability tests , Wing flow method tests

    Lifting-Line Predictions for Induced Drag and Lift in Ground Effect

    Phillips, W. F. / Hunsaker, D. F. | AIAA | 2013
    Schlagwörter: Lifting Line Method , Wing in Ground Effect , Rectangular Wing , Potential Flow

    Dynamic Aeroelasticity of Wings with Tip Propeller by Using Navier–Stokes Equations

    Guruswamy, Guru P. | AIAA | 2019
    Schlagwörter: Rectangular Wing , Wind Tunnel Tests , Potential Flow , Wing Tip

    Insights into the development of the tumble motion using the direct and indirect steady-flow test methods

    Liu, Daming / Jia, Ming / Wang, Tianyou et al. | SAGE Publications | 2014
    Schlagwörter: Steady-flow tests , direct test method

    Investigations into Increasing the Lift of Wings by Boundary Layer Control Through Blowing

    F. Thomas | NTIS | 1967
    Schlagwörter: Wing flaps , Wing slots , Wing flow method tests

    Assessment of body-freedom flutter for an unmanned aerial vehicle

    Schäfer, D. / Vidy, C. / Mack, C. et al. | Springer Verlag | 2018
    Schlagwörter: Potential flow theory , Euler method , Flying wing combat UAV

    Design and Characterization of High-Lift Capabilities for Slotted, Natural-Laminar-Flow Airfoils

    Ortiz-Melendez, Hector D. / Long, Ethan / Colletti, Christopher R. et al. | AIAA | 2023
    Schlagwörter: Aircraft Wing Design , Aircraft Wing Components , Wind Tunnel Tests , Laminar Flow

    Effect of Leading-Edge Cranks on Stability and Control of Active-Flow-Control-Enabled Tailless Aircraft

    Veismann, Marcel / Gharib, Morteza / Taubert, Lutz et al. | AIAA | 2023
    Schlagwörter: Active Flow Control , Flow Separation , Blended Wing Body , Flow Control (Fluid) , Wind Tunnel Tests

    Experimental and Theoretical Flutter Investigation for a Range of Wing Wind-Tunnel Models

    Moradi, Mehrdad / Sadeghi, Morteza H. / Dowell, Earl H. | AIAA | 2017
    Schlagwörter: Compressible Flow , Flow Velocity , Wing Root , Vortex Lattice Method