rdf-syntax-grammar
mods:
  schema location: http://www.loc.gov/mods/v3 http://www.loc.gov/standards/mods/v3/mods-3-2.xsd
  title info:
    non sort: An
    title: approximate integral method for calculating the incompressible laminar boundary layer on an infinite swept wing on which velocity and suction distribution are arbitrary
  name:
    name part: Pinsent, H. G.
    role:
      role term: creator
  name:
    name part: Pinsent, P. A.
  name:
    name part: Aeronautical Research Council (Great Britain)
  type of resource: text
  genre: bibliography
  origin info:
    place:
      place term: enk
    date issued: 1962
    issuance: monographic
  language:
    language term: eng
  physical description:
    form: print
    extent: 38 pages : illustrations ; 28 cm.
  note: by H.G. and P.A. Pinsent.
  note: Cover title.
  note: "February, 1959" -- page [1].
  note: "Previously issued as Handley Page Research Report Number 54--A.R.C. 22,154" -- page [1].
  note: Includes bibliographical references (page 19).
  subject:
    topic: Boundary layer
  subject:
    topic: Airplanes
    topic: Wings, Swept-back
  classification: 629.13432
  related item:
    title info:
      title: Reports and memoranda (Aeronautical Research Council (Great Britain)) ; no. 3241
  record info:
    record content source: UKM
    record creation date: 741222
    record change date: 20151020052347.0
    record identifier: in00001393634