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