Effects of probe size on measurements in a laminar boundary layer in supersonic flow
By: G. R. Ludwig.
Contributors: UTIA
Series: UTIA technical note -- no.9
Publisher: Institute of Aerophysics
Published: 1956
Place of publication: [Downsview, Ont.]
Subjects: Laminar boundary layer; Probes; Supersonic flow
Notes: Includes bibliographical references.