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Volumn 23, Issue 4, 2002, Pages 547-553

Oxidation- and creep-enhanced fatigue of haynes 188 alloy-oxide scale system under simulated pulse detonation engine conditions

Author keywords

Laser high cycle fatigue; Pulse detonation engines; Surface crack initiation and propagation

Indexed keywords

ALLOYS; CARBON DIOXIDE LASERS; COMPUTER SIMULATION; CRACK INITIATION; FATIGUE OF MATERIALS; FATIGUE TESTING; FINITE DIFFERENCE METHOD; LASER PULSES; OXIDES; PULSED LASER APPLICATIONS; TEMPERATURE; THERMAL STRESS;

EID: 0036458191     PISSN: 01966219     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (7)

References (4)
  • 1
    • 85003039504 scopus 로고
    • Review of propulsion applications and numerical simulations of the pulsed detonation engine concept
    • S. Eidelman, W. Grossmann, and I. Lottati, "Review of Propulsion Applications and Numerical Simulations of the Pulsed Detonation Engine Concept," J. Propulsion, vol. 7, pp. 857-865, 1991.
    • (1991) J. Propulsion , vol.7 , pp. 857-865
    • Eidelman, S.1    Grossmann, W.2    Lottati, I.3
  • 4
    • 0012079091 scopus 로고    scopus 로고
    • Laser high-cycle thermal fatigue of pulsed detonation engine combustor materials tested
    • NASA Glenn Research Center, Cleveland, Ohio, NASA TM-210605
    • D. Zhu, D. S. Fox, and R. A. Miller, "Laser High-Cycle Thermal fatigue of Pulsed Detonation Engine Combustor Materials Tested," Research and Technology 2000, NASA Glenn Research Center, Cleveland, Ohio, NASA TM-210605, 2001, 19-22.
    • (2001) Research and Technology 2000 , pp. 19-22
    • Zhu, D.1    Fox, D.S.2    Miller, R.A.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.