Residual strength and crack propagation tests on C-130 airplane center wings with service-imposed fatigue damage / H. Lawrence Snider, Franklin L. Reeder, and William Dirkin.
Fourteen C-130 airplane center wings, each containing service-imposed fatigue damage resulting from 4000 to 13,000 accumulated flight hours, were tested to determine their fatigue crack propagation and static residual strength characteristics. Eight wings were subjected to a two-step constant amplit...
Saved in:
Online Access: |
Link to online resource Search for the full-text version of this title in HathiTrust |
---|---|
Main Author: | |
Corporate Authors: | , , |
Other Authors: | , |
Format: | Government Document Book |
Language: | English |
Published: |
Washington, D.C. : Springfield, Va. :
National Aeronautics and Space Administration ; For sale by the National Technical Information Service [distributor],
1972.
|
Series: | NASA contractor report ;
NASA CR-2075. |
Subjects: |
Internet
Link to online resourceSearch for the full-text version of this title in HathiTrust
Norlin Library - Government Information - US
Call Number: |
NAS 1.26:2075
|
---|---|
NAS 1.26:2075 | Available Place a Hold |