View source for 2023 Boeing IRAD Testing

{| class="wikitable" style="width: 50%;"
|-
|'''Point of Contact:'''  ''Moises Ocasio''
|-
|'''Description:''' A spike overload test was conducted on 7075-T6 to improve the understanding of crack growth rate constraint-loss behavior as a function of thickness and finite width effects.  
|-
|'''Data that is made available:'''
*7075-T6 Spike Overload Test
|}

{| class="wikitable" style="width: 50%;"
|-
|'''Point of Contact:'''  ''Moises Ocasio''
|-
|'''Description:''' A spike overload test was conducted on 7075-T6 to improve the understanding of crack growth rate constraint-loss behavior as a function of thickness and finite width effects.  
|-
|'''Data that is made available:'''
*7075-T6 Spike Overload Test
|}

{| class="wikitable" style="width: 50%;"
|-
|'''Point of Contact:'''  ''Moises Ocasio''
|-
|'''Description:''' A spike overload test was conducted on 7075-T6 to improve the understanding of crack growth rate constraint-loss behavior as a function of thickness and finite width effects.  
|-
|'''Data that is made available:'''
*7075-T6 Spike Overload Test
|}