SCOPUS 정보 검색 플랫폼

Volumn 80, Issue 2, 1989, Pages 147-163

High cycle fatigue in aircraft gas turbines—an industry perspective

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; FATIGUE; TURBINES-GAS;

EID: 0030439336 PISSN: 03769429 EISSN: 15732673 Source Type: Journal
DOI: 10.1007/BF00012667 Document Type: Article

Times cited : (388)

References (14)

1
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- presented at 1995 USAF Structural Integrity Program Conference, San Antonio, Texas, 28–30 November 1995, Document Release ASC 95-2510, WLPOTC, Wright Patterson Air Force Base, Ohio
- (1995) Plan to Control High Cycle Fatigue in Engines
- Huber, N.¹

2
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- Longmans, Green, and Co., London
- (1899) Mechanics Applied to Engineering
- Goodman, J.¹

4
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- J.R. Zuiker and T. Nicholas, On high cycle fatigue design limits under combined high and low cycle fatigue, International Journal of Fatigue (1996).

5
- 85025881466
- M.A. McGaw, S. Kalluri, D. Moore and J. Heine, The Cumulative Fatigue Damage Behavior of MarM247 in Air and High Pressure Hydrogen, Second Symposium on Advances in Fatigue Life Time Predictive Techniques.

6
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- D.P. DeLuca and C.G. Annis, Jr., Fatigue in Single Crystal Nickel Superalloys, Final Contractor Report No. FR23800, United Technologies, Pratt & Whitney, Office of Naval Research, Contract N00014–91-C-0124, (1995).

7
- 84950387449
- On the use of the Goodman diagram for high cycle fatigue design
- (1996) International Journal of Fracture , vol.80 , pp. 219-235
- Nicholas, T.¹ Zuiker, J.R.²

8
- 84950408668
- Air Force Aircraft Jet Engine Manufacturing and Production Processes, Report of the Ad Hoc Committee, United States Air Force Scientific Advisory Board, SAF/AQQS, the Pentagon, Washington DC 20330–1000, (July 1992).

9
- 84950408669
- Engine Structural Integrity Program (ENSIP), MIL-STD-1783 (USAF), 30 November 1984.

10
- 0024054104
- Life prediction in high temperature environments: Overview of a current gas turbine engine approach
- (1988) Materials Science and Engineering A , vol.103 , pp. 63-69
- Cowles, B.A.¹

11
- 84950408670
- D.P. Walls, R.E. deLaneuville and S.E. Cunningham, Damage tolerance based life prediction in gas turbine engine blades under vibratory high cycle fatigue, Transactions of the ASME, to appear.

12
- 0346806611
- WRDC-TR-89-4085, Materials Laboratory, Wright Research and Development Center, Air Force Systems Command, Wright-Patterson Air Force Base, Ohio
- (1989) Threshold Fatigue Crack Growth Behavior
- Haake, F.K.¹ Salivar, G.C.² Hindle, E.H.³ Fischer, J.W.⁴ Annis, C.G.⁵

13
- 0029380107
- Mechanisms of fretting fatigue
- (1995) Japan Society of Mechanical Engineers International Journal, Series A , vol.38 , Issue.4 , pp. 403-415
- Mutoh¹

14
- 0030439748
- An assessment of the role of near-threshold crack growth in high-cycle-fatigue life prediction of aerospace titanium alloys under turbine engine spectra
- (1996) International Journal of Fracture , vol.80 , pp. 237-255
- Larsen, J.M.¹ Worth, B.O.² Annis, C.G.³ Haake, F.K.⁴

* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.