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

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

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