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

author
inLanguage
  • en
isPartOf
name
  • 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
P60049

Instances

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

datePublished
  • 1964
description
  • kuvitettu
identifier
  • propertyID: FI-FENNI value: 264460
  • propertyID: FI-MELINDA value: 003180059
  • propertyID: skl value: f640236
isPartOf
name
  • 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
numberOfPages
  • 69 s., 1 liiteluettelo
P60048
P60050
publication
  • location: Helsinki organizer: Suomen teknillisten tieteiden akatemia Teknillisten tieteiden akatemia
publisher

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