Investigation of Boundary Layer Transition in Hypersonic Flow at Angle of Attack

Item

Title
Investigation of Boundary Layer Transition in Hypersonic Flow at Angle of Attack
Date
1966
Index Abstract
Coming Soon
Photo Quality
Complete
Report Number
AFFDL TR 66-122
Creator
Nagel, A. L.
Savage, R. T.
Wanner, R.
Blank, R. W.
Corporate Author
The Boeing Company
Laboratory
Air Force Flight Dynamics Laboratory
Extent
204
Identifier
AD0803781
Access Rights
Export Controls
Distribution Classification
1
Contract
AF 33(615)-2011
DoD Project
1366
DoD Task
136606
DTIC Record Exists
No
Distribution Change Authority Correspondence
AFFDL LTR
Report Availability
Full text available
Date Issued
1966-08
Abstract
The abstract for this report is either unavailable or has yet to be entered
Provenance
AFRL/VACA
Type
report
Format
1 online resource