columbus · Sonic Fatigue Tolerance of Glass Filament Structure: Experimental Results

Sonic Fatigue Tolerance of Glass Filament Structure: Experimental Results

Title: Sonic Fatigue Tolerance of Glass Filament Structure: Experimental Results
Date: 1966
Index Abstract: Coming Soon
Photo Quality: Complete
Report Number: AFFDL TR 66-78
Creator: Hayes, J. A.
Corporate Author: North American Aviation, Inc.
Laboratory: Air Force Flight Dynamics Laboratory
Extent: 168
Identifier: AD0810558
Access Rights: Export Controls
Distribution Classification: 1
Contract: AF 33(615)-2638
DoD Project: 1471
DoD Task: 147101
DTIC Record Exists: No
Distribution Change Authority Correspondence: AFFDL LTR
Report Availability: Full text available
Date Issued: 1966-12
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