Project Reports

• C-130 Hercules

  • Metallurgical Failure Analysis of C-130 Part Number 372903-1R T9936A

• T-34

  • Metallurgical Failure Analysis of T-34 Lower Rear Spar at Wing Station 66

• E-8C JSTARS

  • Fatigue Performance of E-8C Exfoliated Upper Wing Skin Material

  • E-8/B-707 Wing Station 320 Transition Fit Fastener Finite Element Analysis

• General Research

  • Stress Concentration Factor Determination for Various Tensile Test Specimen Configurations by the Finite Element Metod Using MSC/Patran and MSC/Nastran

  The Effects of Truncation and Marker Loads on Spectrum Fatigue Crack Growth

  Bonded Repair of Corrosion Grind-Outs

 

 

 

For copies of completed project reports, please email

castle@usafa.af.mil

USAFA Center for Aircraft Structural Life Extension
HQ USAFA/DFEM
2354 Fairchild Dr, Suite 6H2
USAF Academy CO 80840-6240
Phone:  (719) 333-3618
Fax:  (719) 333-2944
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Last updated 23 October 2006
castle@usafa.af.mil