Skip to main content
Fachgebiete
Automobil + Motoren Bauwesen + Immobilien Business IT + Informatik Elektrotechnik + Elektronik Energie + Nachhaltigkeit Finance + Banking Management + Führung Marketing + Vertrieb Maschinenbau + Werkstoffe Versicherung + Risiko
DE
EN
Themenseiten
Organisationspsychologie Projektmanagement Marketing Smart Manufacturing
Bücher
Zeitschriften
Weitere Formate
Podcasts Webinare Technik Webinare Wirtschaft Kongresse Veranstaltungskalender Awards
Jetzt Einzelzugang starten
Zugang für Unternehmen
Referenzkunden
ATZ-Fachkongress

Chassis.tech plus 2024


4 Kongresse in einer Veranstaltung

Treffen Sie in München die Fachleute von Chassis, Lenkung, Bremsen sowie Reifen/Räder.
Erweiterte Suche
Anmelden
nach oben
Strength of Materials
Erschienen in: Strength of Materials 4/2015

01.07.2015

Fatigue Crack Growth Kinetics in D16AT Aluminum Alloy Specimens with Multiple Stress Concentrators

verfasst von: S. R. Ignatovich, E. V. Karan

Erschienen in: Strength of Materials | Ausgabe 4/2015

Einloggen

Aktivieren Sie unsere intelligente Suche, um passende Fachinhalte oder Patente zu finden.

search-config
loading …

Abstract

The fatigue crack growth in D16AT aluminum alloy specimens with multiple stress concentrators in the form of holes is investigated experimentally. A generalized kinetic fatigue crack growth curve is obtained and the Paris equation coefficients are determined for a great number of cracks. It is shown that a general linear, semi-logarithmic relationship exists between these coefficients for aluminum alloys D16AT, 2024-T3, and 7075-T6. The statistical description of the fatigue crack growth based on the Paris equation is specified by the distribution of the exponent m, which is log-normal for aluminum alloys whose numerical characteristics are common to all types of alloys.
Vorheriger Artikel Fatigue Life Prediction of Titanium Alloys Effected by Process Factors
Nächster Artikel Procedure of Evaluation of Endurance Limit for Welded Joints with Different Width After High-Frequency Mechanical Peening

Sie haben noch keine Lizenz? Dann Informieren Sie sich jetzt über unsere Produkte:

Springer Professional "Wirtschaft+Technik"

Online-Abonnement

Mit Springer Professional "Wirtschaft+Technik" erhalten Sie Zugriff auf:

  • über 102.000 Bücher
  • über 537 Zeitschriften

aus folgenden Fachgebieten:

  • Automobil + Motoren
  • Bauwesen + Immobilien
  • Business IT + Informatik
  • Elektrotechnik + Elektronik
  • Energie + Nachhaltigkeit
  • Finance + Banking
  • Management + Führung
  • Marketing + Vertrieb
  • Maschinenbau + Werkstoffe
  • Versicherung + Risiko

Jetzt Wissensvorsprung sichern!

Jetzt informieren

Springer Professional "Technik"

Online-Abonnement

Mit Springer Professional "Technik" erhalten Sie Zugriff auf:

  • über 67.000 Bücher
  • über 390 Zeitschriften

aus folgenden Fachgebieten:

  • Automobil + Motoren
  • Bauwesen + Immobilien
  • Business IT + Informatik
  • Elektrotechnik + Elektronik
  • Energie + Nachhaltigkeit
  • Maschinenbau + Werkstoffe




 

Jetzt Wissensvorsprung sichern!

Jetzt informieren
Literatur
1.
J. Schijve, “Multiple-site damage in aircraft fuselage structures,” Fatigue Fract. Eng. Mater. Struct., 18, No. 3, 329–344 (1995).CrossRef
2.
U. G. Goranson, Damage Tolerance. Facts and Fiction, Keynote Presentation in Int. Conf. on Damage Tolerance of Aircraft Structure (Sept. 25, 2007, Delft).
3.
T. Swift, “Widespread fatigue damage monitoring – issues and concerns,” in: Proc. of 5th Int. Conf. on Structural Airworthiness New and Aging Aircraft (June 16–18, 1993, Hamburg, Germany) (1993), pp. 829–870.
4.
P. Tong, R. Greif, and L. Chen, “Residual strength of aircraft panels with multiple site damage,” Comput. Mech., 13, No. 4, 285–294 (1994).CrossRef
5.
S. R. Ignatovich, “Probabilistic model of multiple-site fatigue damage of riveting in airframes,” Strength Mater., 46, No. 3, 336–344 (2014).CrossRef
6.
Recommendations for Regulatory Action to Prevent Widespread Fatigue Damage in the Commercial Airplane Fleet, Final Report of the AAWG (1999).
7.
C. Proppe, “Probabilistic analysis of multi-site damage in aircraft fuselages,” Comput. Mech., 30, No. 4, 323–329 (2003).CrossRef
8.
G. Cavallini and R. Lazzeri, “A probabilistic approach to fatigue design of aerospace components by using the risk assessment evaluation,” in: Ramesh K. Agarwal (Ed.), Recent Advances in Aircraft Technology, InTech (2012), pp. 29–48.
9.
H. L. Wang and A. F. Grandt, “Monte Carlo analysis of widespread fatigue damage in lap joints,” in: Analysis of Widespread Fatigue Damage in Aerospace Structures (Final Report for Air Force Office of Scientific Research), Prep. by A. F. Grandt, Jr., T. N. Farris, and B. H. Hillberry, Purdue University (1999).
10.
V. V. Panasyuk, Limit Equilibrium of Cracked Brittle Bodies [in Russian], Naukova Dumka, Kiev (1968).
11.
A. Carpinteri, Handbook of Fatigue Crack Propagation in Metallic Structures, Elsevier Science BV, Amsterdam (1994).
12.
G. C. Salivar, J. N. Yang, and B. J. Schwartz, “A statistical model for the prediction for fatigue crack growth under a block type spectrum loading,” Eng. Fract. Mech., 31, No. 3, 371–380 (1988).CrossRef
13.
J. N. Yang, W. H. Hsi, S. D. Manning, and J. K. Rudd, “Stochastic crack propagation in fastener holes,” J. Aircraft, 22, No. 9, 810–817 (1982).CrossRef
14.
S. Pattabhiraman, N. H. Kim, and R. T. Haftka, “Effects of uncertainty reduction measures by structural health monitoring on safety and lifecycle cost of airplanes,” in: Proc. of 5lst Conf. “AIAA/ASME/ASCE/ANS/ASC Structures, Structural Dynamics and Materials” (Apr. 12–15, 2010, Orlando, Florida, USA) (2010), Vol. 3, pp. 2221–2232.
15.
S. Pattabhiraman, R. T. Haftka, and N. H. Kim, “Effect of inspection strategies on the weight and lifecycle cost of airplanes,” in: Proc. of 52nd Conf. “AIAA/ASME/ASCE/ANS/ASC Structures, Structural Dynamics and Materials” (Apr. 4–7, 2011, Denver, Colorado, USA) (2011), Vol. 2, pp. 900–913.
16.
J. C. Newman, Jr., E. P. Phillips, and M. H. Swain, “Fatigue-life prediction methodology using small-crack theory,” Int. J. Fatigue, 21, No. 2, 109–119 (1999).CrossRef
17.
A. Coppe, R. T. Haftka, N. H. Kim, and F.-G. Yuan, “Statistical characterization of damage propagation properties in structural health monitoring,” in: Proc. of 50th Conf. “AIAA Non-Deterministic Approaches” (May 4–7, 2009, Palm Springs, CA, USA) (2009), Vol. 4, pp. 1988–1997.
18.
A. Coppe, R. T. Haftka, N. H. Kim, and F.-G. Yuan, “Uncertainty reduction of damage growth properties using structural health monitoring,” J. Aircraft, 47, No. 6, 2030–2038 (2010).CrossRef
19.
A. A. Kale and R. T. Haftka, “Tradeoff of weight and inspection cost in reliability-based structural optimization,” J. Aircraft, 45, No. 1, 77–85 (2008).CrossRef
20.
G. B. Sinclair and R. V. Pierie, “On obtaining fatigue crack growth parameters from the literature,” Int. J. Fatigue, 12, No. 1, 57–62 (1990).CrossRef
21.
E. V. Karan, “Procedure of the investigation on the multiple fatigue damage of specimens with holes,” Naukoemni Tekhnol., 21, No. 1, 105–109 (2014).
22.
A. Rambalakos and G. Deodatis, “Non-periodic inspection of aging aircraft structures,” in: Proc. of 9th Joint FAA/DoD/NASA Conf. on Aging Aircraft (March 6–9, 2006, Atlanta, GA, USA) (2006), pp. 1–18.
23.
P. Romvari, L. Toth, and D. Nad’, “Analysis of irregularities in the distribution of fatigue cracks in metals,” Strength Mater., 12, No. 12, 1481–1491 (1980).CrossRef
24.
M. Baker and I. Stanley, Assessing and Modelling the Uncertainty in Fatigue Crack Growth in Structural Steels, HSE Research Report RR643 (2008).
Metadaten
Titel
Fatigue Crack Growth Kinetics in D16AT Aluminum Alloy Specimens with Multiple Stress Concentrators
verfasst von
S. R. Ignatovich
E. V. Karan
Publikationsdatum
01.07.2015
Verlag
Springer US
Erschienen in
Strength of Materials / Ausgabe 4/2015
Print ISSN: 0039-2316
Elektronische ISSN: 1573-9325
DOI
https://doi.org/10.1007/s11223-015-9694-3

Weitere Artikel der Ausgabe 4/2015

Strength of Materials 4/2015 Zur Ausgabe

SCIENTIFIC AND TECHNICAL SECTION

Methodology of Including Spatial Nonuniformity of Material Properties in the Brittle Fracture Resistance Calculation for WWER-1000 Reactor Pressure Vessels. Part 2. Experimental Investigations

OriginalPaper

A Study of the Dynamic Characteristics of the Cyclone-4 Launch Vehicle on the Basis of a Continuum Rod Model

OriginalPaper

Influence of the Exciting Force Application Point on the Amplitude Spectrum of Flexural Vibrations in a Beam with a “Breathing” Crack

OriginalPaper

Computational-Experimental Investigation of Fracture Toughness in Longitudinal Shear

OriginalPaper

Bayesian Estimation Under Constant-Stress Partially Accelerated Life Test for Pareto Distribution with Type-I Censoring

OriginalPaper

Numerical Procedure of Determining the Effective Mechanical Characteristics of an Aligned Fiber Composite

Premium Partner

    Marktübersichten

    Die im Laufe eines Jahres in der „adhäsion“ veröffentlichten Marktübersichten helfen Anwendern verschiedenster Branchen, sich einen gezielten Überblick über Lieferantenangebote zu verschaffen. 

    Zur Marktübersicht
    Bildnachweise