The unsteady laminar boundary layer on an axisymmetric body subject to small amplitude fluctuations in the free-stream velocity
By: Peter W. Duck.
Contributors: Institute for Computer Applications in Science and Engineering.
Series: ICASE report -- 91-50.; NASA contractor report -- 187579.; NASA contractor report -- NASA CR-187579.
Publisher: National Aeronautics and Space Administration, Langley Research Center, Institute for Computer Applications in Science and Engineering; For sale by the National Technical Information Service
Published: 1991
Place of publication: Hampton, Va; [Springfield, Va
Language: eng
Format: Microform
Subjects: Boundary layer.; Axisymmetric bodies.; Circular cylinders.; Eigenvalues.; Flow velocity.; Free flow.; Laminar boundary layer.; Unsteady flow.
Notes: Also available via Internet from the NASA Technical Report Server web site. Address as of 4/11/05: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19910017807%5F1991017807.pdf; current access is available via PURL.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1991]. 1 microfiche.