Numerical investigation of unsteady laminar incompressible co-axial boundary layer flows
by Urmila Agarwal and T. Paul Torda. Prepared by Illinois Institute of Technology, Chicago, Ill., for Lewis Research Center.

Description

Main Author

Agarwal, Urmila.

Related Names

Torda, T. Paul.
United States. National Aeronautics and Space Administration.
Lewis Research Center.
Illinois Institute of Technology.

Language(s)

English

Published

Washington, National Aeronautics and Space Administration; 1967.

Subjects

Nuclear rockets.
Laminar flow.
Boundary layer.

Note

NASA CR-908.

Physical Description

xii, 122 p. : illus.

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