10 research outputs found

    A validation of LTRAN2 with high frequency extensions by comparisons with experimental measurements of unsteady transonic flows

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    A high frequency extension of the unsteady, transonic code LTRAN2 was created and is evaluated by comparisons with experimental results. The experimental test case is a NACA 64A010 airfoil in pitching motion at a Mach number of 0.8 over a range of reduced frequencies. Comparisons indicate that the modified code is an improvement of the original LTRAN2 and provides closer agreement with experimental lift and moment coefficients. A discussion of the code modifications, which involve the addition of high frequency terms of the boundary conditions of the numerical algorithm, is included

    Validation of LTRAN2-HI by comparison with unsteady transonic experiment

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    A hybrid shear panel

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    Targeted radionuclide therapy of cancer

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