Subsonic tests in free molecule flow on impact tube pressure probes having a wide range of tube lengths at angles of attack up to 90 degrees
By: Peter C. Hughes.
Contributors: UTIAS
Series: UTIAS technical note -- no.92
Publisher: Institute for Aerospace Studies
Published: 1965
Place of publication: [Downsview, Ont.]
Number of pages: 21
Subjects: Free molecular flow; Probes
Notes: Includes bibliographical references.