Evaluation of Sc-bearing aluminum alloy C557 for aerospace applications

Materials Science Forum

Volumn 396-402, Issue 2, 2002, Pages 839-844

  Domack, M S ^a   Dicus, D L ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

Al Mg Sc alloys; C557; Fracture toughness; Tensile; Thermal exposure

Indexed keywords

AEROSPACE APPLICATIONS; CORROSION RESISTANCE; SCANDIUM; STRENGTH OF MATERIALS; TEXTURES; THERMODYNAMIC STABILITY;

AIRFRAME STRUCTURAL APPLICATIONS;

ALUMINUM ALLOYS;

EID: 0036435383     PISSN: 02555476     EISSN: 16629752     Source Type: Book Series    
DOI: 10.4028/www.scientific.net/msf.396-402.839     Document Type: Conference Paper

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