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
An edition of 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 (1965)
By Hughes, Peter C.
Publish Date
1965
Publisher
Institute for Aerospace Studies
Language
-
Pages
21
1-1 of 1 Editions
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
Pages: 21
Published In: 1965
Publisher: Institute for Aerospace Studies