A shock tube technique to determine steady-flow losses of orifices and other duct elements
By: George Rudinger.
Contributors: Cornell Aeronautical Laboratory
Series: Project SQUID report -- no. CAL-77-P
Publisher: Cornell Aeronautical Laboratory
Published: 1958
Place of publication: Buffalo, N.Y
Number of pages: 19
Notes: Bibliographical references: p. 18-19.

Contract number: Nonr-1858(25)