[
    {
        "id": "authors:htf3g-dcx05",
        "collection": "authors",
        "collection_id": "htf3g-dcx05",
        "cite_using_url": "https://resolver.caltech.edu/CaltechAUTHORS:20210603-160013203",
        "type": "article",
        "title": "An empirical correlation between lift and the properties of leading-edge vortices",
        "author": [
            {
                "family_name": "Jardin",
                "given_name": "T.",
                "orcid": "0000-0001-9704-2984",
                "clpid": "Jardin-Thierry"
            },
            {
                "family_name": "Choi",
                "given_name": "J.",
                "clpid": "Choi-Jeesoon"
            },
            {
                "family_name": "Colonius",
                "given_name": "T.",
                "orcid": "0000-0003-0326-3909",
                "clpid": "Colonius-T"
            }
        ],
        "abstract": "Using data from numerical simulations, we show that the lift experienced by both impulsively started and surging airfoils correlates well with the sum of the circulation of the leading-edge vortices truncated at the trailing edge. Therefore, we suggest that reasonable estimates of the lift can be obtained using only two vortex parameters, i.e., its circulation and its position. In addition to being convenient for non-intrusive estimation of forces from PIV measurements, we show that this approach can be used to derive low-order models for the analysis of vortex-lift configurations. In particular, we apply this correlation to model high-amplitude surging, which allows us to quantify the effect of wake-capture mechanisms and to determine the flow parameters that drive optimal lift.",
        "doi": "10.1007/s00162-021-00567-x",
        "issn": "0935-4964",
        "publisher": "Springer",
        "publication": "Theoretical and Computational Fluid Dynamics",
        "publication_date": "2021-08",
        "series_number": "4",
        "volume": "35",
        "issue": "4",
        "pages": "437-448"
    },
    {
        "id": "authors:wb377-d7a14",
        "collection": "authors",
        "collection_id": "wb377-d7a14",
        "cite_using_url": "https://resolver.caltech.edu/CaltechAUTHORS:20150420-134149863",
        "type": "article",
        "title": "Surging and plunging oscillations of an airfoil at low Reynolds number",
        "author": [
            {
                "family_name": "Choi",
                "given_name": "Jeesoon",
                "clpid": "Choi-Jeesoon"
            },
            {
                "family_name": "Colonius",
                "given_name": "Tim",
                "orcid": "0000-0003-0326-3909",
                "clpid": "Colonius-T"
            },
            {
                "family_name": "Williams",
                "given_name": "David R.",
                "clpid": "Williams-D-R"
            }
        ],
        "abstract": "We investigate the forces and unsteady flow structures associated with harmonic oscillations of an airfoil in the streamwise (surging) and transverse (plunging) directions in two-dimensional simulations at low Reynolds number. For the surging case, we show that there are specific frequencies where the wake instability synchronizes with the unsteady motion of the airfoil, leading to significant changes in the mean forces. Resonant behaviour of the time-averaged forces is observed near the vortex shedding frequency and its subharmonic; the behaviour is reminiscent of the dynamics of the generic nonlinear oscillator known as the Arnol'd tongue or the resonance horn. Below the wake instability frequency, there are two regimes where the fluctuating forces are amplified and attenuated, respectively. A detailed study of the flow structures associated with leading-edge vortex (LEV) growth and detachment are used to relate this behaviour with the LEV acting either in phase with the quasi-steady component of the forces for the amplification case, or out of phase for the attenuation case. Comparisons with wind tunnel measurements show that phenomenologically similar dynamics occur at higher Reynolds number. Finally, we show that qualitatively similar phenomena occur during both surging and plunging.",
        "doi": "10.1017/jfm.2014.674",
        "issn": "0022-1120",
        "publisher": "Cambridge University Press",
        "publication": "Journal of Fluid Mechanics",
        "publication_date": "2015-01",
        "volume": "763",
        "pages": "237-253"
    }
]