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

Item

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