Damage Tolerance in Aircraft Structures
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TOTAL DOCUMENTS

12

(FIVE YEARS 0)

H-INDEX

6

(FIVE YEARS 0)

Published By ASTM International

9780803100312

Latest Documents Most Cited Documents Contributed Authors Related Sources Related Keywords

The Significance of Fatigue Crack Closure

Damage Tolerance in Aircraft Structures ◽

10.1520/stp26680s ◽

2009 ◽

pp. 230-230-13 ◽

Author(s):

W Elber

Keyword(s):

Fatigue Crack ◽

Crack Closure ◽

Fatigue Crack Closure

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Initiation and Growth of Fatigue Cracks in and Residual Strength of the F-100 Wing

Damage Tolerance in Aircraft Structures ◽

10.1520/stp26677s ◽

2009 ◽

pp. 144-144-20 ◽

Author(s):

WD Graziano ◽

GE Fitch

Keyword(s):

Residual Strength ◽

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Evaluation and Prediction of the Residual Strength of Center Cracked Tension Panels

Damage Tolerance in Aircraft Structures ◽

10.1520/stp26673s ◽

2009 ◽

pp. 50-50-29 ◽

Author(s):

CE Feddersen

Keyword(s):

Residual Strength

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Development of the Fail-safe Design Features of the DC-10

Damage Tolerance in Aircraft Structures ◽

10.1520/stp26678s ◽

2009 ◽

pp. 164-164-51 ◽

Author(s):

T Swift

Keyword(s):

Design Features ◽

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Fatigue Crack Propagation in Stiffened Panels

Damage Tolerance in Aircraft Structures ◽

10.1520/stp26674s ◽

2009 ◽

pp. 79-79-19 ◽

Author(s):

CC Poe

Keyword(s):

Fatigue Crack ◽

Crack Propagation ◽

Fatigue Crack Propagation ◽

Stiffened Panels

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Effect of Thickness on the Fracture Toughness of 7075 Aluminum in the T6 and T73 Conditions

Damage Tolerance in Aircraft Structures ◽

10.1520/stp26671s ◽

2009 ◽

pp. 16-16-23 ◽

Author(s):

FC Allen

Keyword(s):

Fracture Toughness

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The Dependence of Fatigue Crack Propagation on Strain Energy Release Rate and Crack Opening Displacement

Damage Tolerance in Aircraft Structures ◽

10.1520/stp26670s ◽

2009 ◽

pp. 1-1-15 ◽

Author(s):

JM Barsom

Keyword(s):

Fatigue Crack ◽

Crack Propagation ◽

Energy Release Rate ◽

Energy Release ◽

Crack Opening Displacement ◽

Fatigue Crack Propagation ◽

Release Rate ◽

Crack Opening ◽

Strain Energy Release ◽

Opening Displacement

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The Ballistic Damage Characteristics and Damage Tolerance of Wing Structural Elements

Damage Tolerance in Aircraft Structures ◽

10.1520/stp26679s ◽

2009 ◽

pp. 215-215-15 ◽

Author(s):

JE Jensen

Keyword(s):

Damage Tolerance ◽

Structural Elements ◽

Damage Characteristics

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An Approach to Predicting the Growth to Failure of Fatigue Cracks Subjected to Arbitrary Uniaxial Cyclic Loading

Damage Tolerance in Aircraft Structures ◽

10.1520/stp26676s ◽

2009 ◽

pp. 122-122-22 ◽

Author(s):

TR Brussat

Keyword(s):

Cyclic Loading ◽

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Material Toughness and Residual Strength of Damage Tolerant Aircraft Structures

Damage Tolerance in Aircraft Structures ◽

10.1520/stp26675s ◽

2009 ◽

pp. 98-98-24 ◽

Author(s):

AF Liu ◽

JC Ekvall

Keyword(s):

Residual Strength ◽

Aircraft Structures ◽

Damage Tolerant

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