Development of an advanced panel method for complex configurations in subsonic compressible flow; application to the computation of the potential flow through ducts
By: C. M. van Beek.
Contributors: National Aerospace Laboratory (The Netherlands)
Publisher: National Aerospace Laboratory
Published: 1987
Place of publication: Amsterdam, Netherlands
Number of pages: 45
Subjects: Ducted flow; Panel method
Notes: Includes bibliographical references: p. 26-27.