Numerical investigation of unsteady laminar incompressible co-axial boundary layer flows
By: by Urmila Agarwal and T. Paul Torda. Prepared by Illinois Institute of Technology, Chicago, Ill., for Lewis Research Center
Contributors: Torda, T. Paul; Illinois Institute of Technology; Lewis Research Center; United States. National Aeronautics and Space Administration
Publisher: National Aeronautics and Space Administration; For sale by the Clearinghouse for Federal Scientific and Technical Information
Published: 1967
Place of publication: Washington; Springfield, Va
Language: eng
Number of pages: 122
Subjects: Boundary layer; Laminar flow; Nuclear rockets
Notes: NASA CR-908.

Bibliography: p. 120-122.