An application of integral transformations and the Wiener-Hopf technique to the supersonic flow past on oscillating, nearly circular, slender body and past an elastic, two-dimensional, thin wing
An application of integral transformations and the Wiener-Hopf technique to the supersonic flow past on oscillating, nearly circular, slender body and past an elastic, two-dimensional, thin wing
An application of integral transformations and the Wiener-Hopf technique to the supersonic flow past on oscillating, nearly circular, slender body and past an elastic, two-dimensional, thin wing
An application of integral transformations and the Wiener-Hopf technique to the supersonic flow past on oscillating, nearly circular, slender body and past an elastic, two-dimensional, thin wing