Works matching DE "AIRFRAME fatigue"

Results: 38

Conceptual design and sizing of airframe panels according to safe-life acoustic fatigue criteria.

Published in:

Aeronautical Journal, 2011, v. 115, n. 1163, p. 15, doi. 10.1017/S0001924000005339

By:

Ajaj, R. M.;
Allegri, G.;
Isikveren, A. T.

Publication type:

Article

Probabilistic Model of Multiple-Site Fatigue Damage of Riveting in Airframes.

Published in:

Strength of Materials, 2014, v. 46, n. 3, p. 336, doi. 10.1007/s11223-014-9555-5

By:

Ignatovich, S.

Publication type:

Article

Aviation Accident Causation Analysis Based on Complex Network Theory.

Published in:

Transactions of Nanjing University of Aeronautics & Astronautics, 2021, v. 38, n. 4, p. 646, doi. 10.16356/j.1005⁃1120.2021.04.011

By:

YUE Rentian;
LI Junwei;
HAN Meng

Publication type:

Article

Reliability of Fatigue-Prone Airframe.

Published in:

International Review of Aerospace Engineering, 2009, v. 2, n. 3, p. 145

By:

Paramonov, Yuri;
Kuznetsov, Aridrey

Publication type:

Article

Damage tolerance analysis of aircraft reinforced panels.

Published in:

Fracture & Structural Integrity, 2011, v. 5, p. 34, doi. 10.3221/IGF-ESIS.16.04

By:

Carta, F.;
Pirondi, A.

Publication type:

Article

Planning Inspections in the Case of Damage Tolerance Approach to Service of Fatigued Aircraft Structures.

Published in:

International Journal of Performability Engineering, 2011, v. 7, n. 3, p. 1

By:

Nechval, N.;
Nechval, K.;
Purgailis, M.;
Strelchonok, V.

Publication type:

Article

Total Fatigue Life Estimation of Notched Structural Components Using Low-Cycle Fatigue Properties.

Published in:

Strain, 2011, v. 47, p. 341, doi. 10.1111/j.1475-1305.2010.00775.x

By:

Maksimovic, S.;
Posavljak, S.;
Maksimovic, K.;
Nikolic, V.;
Djurkovic, V.

Publication type:

Article

Effect of Temperature on the Residual Stresses in an Integral Structure with a Crack-Retarding Patch.

Published in:

Strain, 2011, v. 47, p. 293, doi. 10.1111/j.1475-1305.2010.00768.x

By:

Liljedahl, C. D. M.;
Fitzpatrick, M. E.;
Zanellato, O.;
Edwards, L.

Publication type:

Article

Principal Component Analysis of Acoustic Emission Signals From Landing Gear Components: An Aid to Fatigue Fracture Detection.

Published in:

Strain, 2011, v. 47, p. e588, doi. 10.1111/j.1475-1305.2009.00661.x

By:

Eaton, M. J.;
Pullin, R.;
Hensman, J. J.;
Holford, K. M.;
Worden, K.;
Evans, S. L.

Publication type:

Article

A crack growth–based individual aircraft monitoring method utilising a damage metric.

Published in:

Structural Health Monitoring, 2018, v. 17, n. 5, p. 1178, doi. 10.1177/1475921717738389

By:

White, Paul;
Mongru, David;
Molent, Lorrie

Publication type:

Article

Structural Health Monitoring, In-service Experience, Benefit and Way Ahead.

Published in:

Structural Health Monitoring, 2010, v. 9, n. 3, p. 209, doi. 10.1177/1475921710366655

By:

Stolz, Christian;
Neumair, Manfred

Publication type:

Article

Analysis of crack interactions at adjacent holes and onset of multi-site fatigue damage in aging airframes.

Published in:

International Journal of Fracture, 2009, v. 156, n. 2, p. 155, doi. 10.1007/s10704-009-9354-3

By:

Wang, X.;
Modarres, M.;
Hoffman, P.

Publication type:

Article

Aircraft Duraluminum Wing Spar Fatigue Testing.

Published in:

FME Transactions, 2017, v. 45, n. 4, p. 531, doi. 10.5937/fmet1704531P

By:

Petrašinović, Nikola;
Petrašinović, Danilo;
Rašuo, Boško;
Milković, Dragan

Publication type:

Article

Adaptive landing gear: Optimum control strategy and potential for improvement.

Published in:

Shock & Vibration, 2009, v. 16, n. 2, p. 175

By:

Mikułowski, Grzegorz;
Jankowski, Łukasz

Publication type:

Article

Dynamical modelling, stochastic simulation and optimization in the context of damage tolerant design.

Published in:

Shock & Vibration, 2006, v. 13, n. 3, p. 445, doi. 10.1155/2006/431319

By:

Butkewitsch, Sergio

Publication type:

Article

Fatigue life recovery in aluminium alloy aircraft structure.

Published in:

Fatigue & Fracture of Engineering Materials & Structures, 2002, v. 25, n. 2, p. 99, doi. 10.1046/j.1460-2695.2002.00481.x

By:

Sharp, P. K;
Liu, Q;
Barter, S. A;
Baburamani, P;
Clark, G

Publication type:

Article

Initiation and early growth of fatigue cracks in an aerospace aluminium alloy.

Published in:

Fatigue & Fracture of Engineering Materials & Structures, 2002, v. 25, n. 2, p. 111, doi. 10.1046/j.1460-2695.2002.00482.x

By:

Barter, S. A;
Sharp, P. K;
Holden, G;
Clark, G

Publication type:

Article

Review of fatigue monitoring of agile military aircraft.

Published in:

Fatigue & Fracture of Engineering Materials & Structures, 2000, v. 23, n. 9, p. 767, doi. 10.1046/j.1460-2695.2000.00330.x

By:

Molent, L.;
Aktepe, B.

Publication type:

Article

NOMINATION OF SPECIFIED LIFE USING BAYES-FIDUCIAL APPROACH.

Published in:

Transport & Engineering, 2008, v. 27, p. 319

By:

Paramonov, Yu

Publication type:

Article

Design and Evaluation of a Wireless Sensor Network Based Aircraft Strength Testing System.

Published in:

Sensors (14248220), 2009, v. 9, n. 6, p. 4195, doi. 10.3390/s90604195

By:

Jian Wu;
Shenfang Yuan;
Genyuan Zhou;
Sai Ji;
Zilong Wang;
Yang Wang

Publication type:

Article

Effect of expansion technique and plate thickness on near-hole residual stresses and fatigue life of cold expanded holes.

Published in:

Journal of Materials Science, 1999, v. 34, n. 6, p. 1243, doi. 10.1023/A:1004521309415

By:

Özdemir, A.;
Hermann, R.

Publication type:

Article

SKIN SURFACE EXTRUSION/INTRUSION STRUCTURE AS AN INDICATOR OF AGING AIRCRAFT FATIGUE.

Published in:

Problems of Friction & Wear, 2018, v. 79, n. 2, p. 78

By:

IGNATOVICH, S.;
KARUSKEVICH, M.;
KORCHUK, O.;
MASLAK, T.;
PYSHCHYK, A.

Publication type:

Article

Improving the fatigue performance of airframe structures by combining geometrical modifications and laser heating.

Published in:

Fatigue & Fracture of Engineering Materials & Structures, 2018, v. 41, n. 5, p. 1183, doi. 10.1111/ffe.12762

By:

Lu, J.;
Huber, N.;
Kashaev, N.

Publication type:

Article

A comparison of fatigue crack growth performance of two aerospace grade aluminium alloys reinforced with bonded crack retarders.

Published in:

Fatigue & Fracture of Engineering Materials & Structures, 2018, v. 41, n. 5, p. 1237, doi. 10.1111/ffe.12744

By:

Syed, A. K.;
Zhang, X.;
Fitzpatrick, M. E.

Publication type:

Article

An overview of fatigue in aircraft structures.

Published in:

Fatigue & Fracture of Engineering Materials & Structures, 2017, v. 40, n. 10, p. 1510, doi. 10.1111/ffe.12631

By:

Tavares, S. M. O.;
Castro, P. M. S. T.

Publication type:

Article

Structural integrity and damage type in military aircraft.

Published in:

Fatigue & Fracture of Engineering Materials & Structures, 2010, v. 33, n. 11, p. 752, doi. 10.1111/j.1460-2695.2010.01486.x

By:

Clark, G.;
Jackson, P.

Publication type:

Article

Crack detection in dielectric objects using electrical capacitance tomography imaging.

Published in:

Insight: Non-Destructive Testing & Condition Monitoring, 2011, v. 53, n. 1, p. 21, doi. 10.1784/insi.2011.53.1.21

By:

Soleimani, M.;
Stewart, V. J.;
Budd, C. J.

Publication type:

Article

NEWSDESK: New Secretary General for FEANI; Ultrafine develops semi-automated rig for inspecting hollow shafts; Your opportunity to influence new radiography standards; GE's Phasor XS provides a 24 carat solution.

Published in:: Insight: Non-Destructive Testing & Condition Monitoring, 2011, v. 53, n. 1, p. 4, doi. 10.1784/insi.2011.53.1.4
Publication type:: Article

Comment.

Published in:

Insight: Non-Destructive Testing & Condition Monitoring, 2008, v. 50, n. 3, p. 114

By:

Georgiou, George

Publication type:

Article

Fatigue Crack Growth Prediction under Spectrum Load Sequence in an Aluminum Alloy by K*-RMS Approach.

Published in:

International Journal of Damage Mechanics, 2008, v. 17, n. 6, p. 477, doi. 10.1177/1056789506069473

By:

Manjunatha, C. M.

Publication type:

Article

TESTING CHARACTERIZATION.

Published in:: Advanced Materials & Processes, 2007, v. 165, n. 5, p. 14
Publication type:: Article

Very High Cycle Fatigue Testing under Spectrum Loading for Endurance Limit Structural Design.

Published in:

Journal of the American Helicopter Society, 2020, v. 65, n. 1, p. 1, doi. 10.4050/JAHS.65.012008

By:

Rusk, David T.;
Taylor, Robert E.;
Pregger, Bruce A.;
Sanchez, Luis J.

Publication type:

Article

Rotorcraft Gross Weight and Center of Gravity Prediction Using Regime Recognition.

Published in:

Journal of the American Helicopter Society, 2015, v. 60, n. 4, p. 1, doi. 10.4050/JAHS.60.042009

By:

Moon, Suresh;
Phan, Nam

Publication type:

Article

Degradation of materials and fatigue durability of aircraft constructions after long-term operation.

Published in:

Materials Science, 2006, v. 42, n. 4, p. 427, doi. 10.1007/s11003-006-0098-1

By:

Ostash, O. P.;
Andreiko, I. M.;
Holovatyuk, Yu. V.

Publication type:

Article

MATHEMATICAL MODELS OF THE CALCULATION OF AIRCRAFT STRUCTURAL RELIABILITY.

Published in:

Aviation (1648-7788), 2011, v. 15, n. 1, p. 11, doi. 10.3846/16487788.2011.566315

By:

Kulyk, Mykola;
Kucher, Olexiy;
Miltsov, Vladimir

Publication type:

Article

ANALYSIS OF REPAIRED GAS TURBINE AND COMPRESSOR BLADES.

Published in:

Aviation (1648-7788), 2008, v. 12, n. 2, p. 46, doi. 10.3846/1648-7788.2008.12.46-50

By:

Tishkunov, Alexander;
Gluhihs, Sergejs;
Korjakins, Aleksandrs;
Popovs, Andris

Publication type:

Article

INSPECTION PROGRAM DEVELOPMENT FOR FATIGUE CRACK GROWTH MODEL WITH TWO RANDOM PARAMETERS.

Published in:

Aviation (1648-7788), 2008, v. 12, n. 2, p. 33, doi. 10.3846/1648-7788.2008.12.33-40

By:

Paramonov, Yuri;
Kuznetsov, Andrey

Publication type:

Article

COMPARISON BETWEEN TWO AND THREE PARAMETERS OF FATIGUE CRACK GROWTH MODELS IN AIRFRAME STRUCTURES.

Published in:

Aviation (1648-7788), 2005, v. 9, n. 2, p. 17, doi. 10.3846/16487788.2005.9635899

By:

Wahab, Muhammad Shujauddin;
Paramonov, Yuri M.

Publication type:

Article