http://www.loc.gov/mods/v3 http://www.loc.gov/standards/mods/v3/mods-3-2.xsd
approximate integral method for calculating the incompressible laminar boundary layer on an infinite swept wing on which velocity and suction distribution are arbitrary
Aeronautical Research Council (Great Britain)
"Previously issued as Handley Page Research Report Number 54--A.R.C. 22,154" -- page [1].
Includes bibliographical references (page 19).
Reports and memoranda (Aeronautical Research Council (Great Britain)) ; no. 3241