Published: January 15, 2002Received: April 24, 2001Available on J-STAGE: June 03, 2009Accepted: April 24, 2001
Advance online publication: -
Revised: -
Correction information
Date of correction: June 03, 2009Reason for correction: -Correction: DTRECEIVEDDetails: Right : 20010424
Date of correction: June 03, 2009Reason for correction: -Correction: TITLEDetails: Wrong : Lecture Right : Applications of Strength Design and Safety Assessment in Machine and Structure
Date of correction: June 03, 2009Reason for correction: -Correction: SUBTITLEDetails: Right : II: Aircraft
Date of correction: June 03, 2009Reason for correction: -Correction: AUTHORDetails: Right : Kenichi KATAYANAGI1), Tetsuya OHNISHI2)
Date of correction: June 03, 2009Reason for correction: -Correction: AFFILIATIONDetails: Right :
1) Oye Div., Churyo Eng., Co.
2) Nagoya Aerospace Systems, Mitsubishi Heavy Industries, Ltd.
Date of correction: June 03, 2009Reason for correction: -Correction: KEYWORDDetails: Right : Static strength, Fatigue strength, Damage tolerance, Safety verification, Civil aircraft
Date of correction: June 03, 2009Reason for correction: -Correction: CITATIONDetails: Right : 1) FAR Part 25, Admt. 25-1 thru 25-98, Federal Aviation Administration, DOT. (1999). 3) Military Handbook-5, “Metallic Materials and Element for Aerospace Vehicle Structures” (1998) Paragraph 9. 1. 6. 5) FAA, DOT., report No. AFS-120-73-2 (1973). 6) Schiitz, Von D., RAE TR 73183 (1973). 7) J. C. Ekvall and L. Young, Journal of Testing and Evaluation, 4-4, 231 (1976). 8) I. I. McNaughton, RAE TR 72056 (1972). 9) Advisory Circular 20-128 (1992).