Compressible Boundary Layer Equations And Stagnation Point Solution With Differences In Thermal And Dynamic Boundary Layer Thicknesses Being Considered

Item

Title
Compressible Boundary Layer Equations And Stagnation Point Solution With Differences In Thermal And Dynamic Boundary Layer Thicknesses Being Considered
Date
1961
Index Abstract
Coming Soon
Photo Quality
Not Needed
Report Number
ASD TR 61-107
Creator
Buck, Melving L.
Corporate Author
Aeronautical Systems Div Wright-Patterson AFB Ohio Flight Control Lab
Laboratory
Flight Dynamics Laboratory
Extent
45
Identifier
AD0268584
Access Rights
OTS
Distribution Classification
1
Contract
Laboratory Research - No Contract
DoD Project
1366
DoD Task
14017
DTIC Record Exists
No
Distribution Change Authority Correspondence
None
Report Availability
Full text available by request
Date Issued
1961-08
Abstract
The abstract for this report is either unavailable or has yet to be entered
Type
report
Provenance
Lockheed Martin Missiles & Fire Control
Format
45 pages ; 28 cm.