columbus · Effects Of The Upstream Influence Of A Shock wave At Supersonic Speeds In The Presence Of A Separated Boundary Layer

Effects Of The Upstream Influence Of A Shock wave At Supersonic Speeds In The Presence Of A Separated Boundary Layer

Title: Effects Of The Upstream Influence Of A Shock wave At Supersonic Speeds In The Presence Of A Separated Boundary Layer
Date: 1954
Index Abstract: Limited
Photo Quality: Undetermined
Report Number: WADC TR 54-31
Creator: Daniels, Lloyd E.; Yoshihara, Hideo
Corporate Author: Aircraft Laboratory
Extent: 31
PB Number: PB133166
Identifier: AD0034209
Distribution Classification: 2
DTIC Record Exists: No
Distribution Change Authority Correspondence: None
Distribution Conflict: Yes
Report Availability: Not available via Contrails
Date Issued: 1954-01
Abstract: The abstract for this report is either unavailable or has yet to be entered
Index In: U.S. Government Research Reports
Type: report