Wind Tunnel Studies Of The Pressure Distribution And The Flow Field In The Wake Of The Lockheed C-141A Starlifter Jet Transport Aircraft

Item

Title
Wind Tunnel Studies Of The Pressure Distribution And The Flow Field In The Wake Of The Lockheed C-141A Starlifter Jet Transport Aircraft
Date
1968
Index Abstract
Not Available
Photo Quality
Complete
Report Number
AFFDL TR 67-163
Creator
Goodrick, T. F.
Corporate Author
Minnesota Univ Minneapolis Dept Of Aeronautics And Engineering Mechanics
Laboratory
Air Force Flight Dynamics Laboratory
Extent
54
Identifier
AD0835380
Access Rights
Export Controls
Distribution Classification
1
Contract
F33615-67-C-1010
DoD Project
6065
DoD Task
606503
DTIC Record Exists
No
Distribution Change Authority Correspondence
AFFDL LTR
Report Availability
Full text available
Date Issued
1968-05
Abstract
The abstract for this report is either unavailable or has yet to be entered
Provenance
Lockheed Martin Missiles & Fire Control
Type
report
Format
1 online resource