Effects of probe tip geometry and size on measurements in a laminary boundary layer in supersonic flow
By: Stanley H. Galezowski.
Contributors: UTIA
Series: UTIA technical note -- no.17
Publisher: Institute of Aerophysics
Published: 1957
Place of publication: [Downsview, Ont.]
Subjects: Laminar boundary layer; Probes
Notes: Includes bibliographical references.