Search Results

You are looking at 1 - 10 of 1,742 items for :

Clear All
Open access

Daniel Krzysztof Dębski

REFERENCES [1] Fatemi A., Yang L.: Cumulative fatigue damage and life prediction theories: a survey of the state of the art for homogeneous materials . Int. J. of Fatigue, vol. 20, nº 1, pp. 9-34, 1998. [2] Schijve, J.: Fatigue of structures and materials in the 20th century and the state of the art . Materials Science, vol. 39, nº 3, pp. 307-333, 2003. [3] Debski M., Debski D.: Selected problems of fatigue strength of aircraft structures. Scientific Library of the Institute of Aviation 36, ISBN 978-83-63539-06-1, Warsaw 2014. [4

Open access

Antoni Niepokólczycki, Andrzej Leski and Krzysztof Dragan

REFERENCES [1] Brzęczek J, Gruszecki H, Pieróg L, Pietruszka J. Selected Aspects Related to Preparation of a Fatigue Test Plan of a Metallic Airframe. Fatigue of Aircraft Structures. Issue 2014. Institute of Aviation Scientific Publications, Warsaw, Poland. [2] Brzęczek J, Gruszecki H, Pieróg L, Pietruszka J. Selected Aspects Related to Preparation of Fatigue Tests of a Metallic Airframe. Fatigue of Aircraft Structures. Issue 2014. Institute of Aviation Scientific Publications, Warsaw, Poland. [3] Brzęczek J, Chodur J, Pietruszka J

Open access

Sung-Jo Park and Hyun-Woo Lee

References AWS., 1987. Welding Handbook, Volume 1. 8th ed. pp.231-233. Bannantine, J.A., Comer, J.J. and Handrock, J.L., 1990. Fundamentals of Metal Fatigue Analysis. Prentice-Hall, Inc. Gurney, T.R., 1979. Fatigue of Welded Structure. 2nd ed. Cambridge University Press. Kim, H., 1992. A study on the fatigue crack opening behavior of the material with welding residual stress field. PhD. Korea University. Kim, W.S., 1997. Residual Stress & Fatigue strength in Welded Ship Structure

Open access

Andrzej Leski, Sylwester Kłysz, Janusz Lisiecki, Gabriel Gmurczyk, Piotr Reymer, Dariusz Bochenek and Dariusz Zasada

References [1] Barter S.A., Molent L., Wanhill R.J.H.(2009). Marker loads for quantitative fractography of fatigue cracks in aerospace alloys. Proceedings of the 25th ICAF Symposium of the International Committee on Aeronautical Fatigue, Rotterdam, The Netherlands, May 2009, p. 15-54 [2] Wanhill R.J.H., Barter S.A. (1994). NLR Technical Publication TP 94177 U, National Aerospace Laboratory NLR , Amsterdam, 1994. [3] Podskarbi S. (2010). Dokumentacja techniczna z zabudowy czujników tensometrycznych na

Open access

Andrzej Leski, Sławomir Klimaszewski and Marcin Kurdelski

References United States Air Force. (1978, January). Individual Aircraft Tracking Methods for Fighter Aircraft Utilizing Counting Accelerometer Data. Ohio: Air Force Flight Dynamics Lab. Wright-Patterson Air Force Base. (AFFDL-TM-78-1-FBE) FAA. (1973). Fatigue Evaluation of Wing and Associated Structure on Small Airplanes. (AFS-120-73-2) Veldman Ray J. & Peckham C. (1982, October). Loads and Dynamics Branch Structures Division. In Handbook of Military Aircraft Design Normal

Open access

Józef Brzęczek, Jerzy Chodur and Janusz Pietruszka

REFERENCES 1. J. Pietruszka “Full-Scale Fatigue Tests of PZL M28 05 SKYTRUCK Aircraft”. Transactions of Institute of Aviation , 1/2009 (196). Warsaw, 2009. 2. J. Brzęczek, J. Chodur, J. Pietruszka “Selected Aspects Related to Metallic Airframe Fatigue Tests Preparation”. Fatigue of Aircraft Structures , Issue 2014, Institute of Aviation. Warsaw, 2015.

Open access

Shashidhar K Kudari and C. M. Sharanaprabhu

of Aircraft Structures, Atlanta, Georgia, (Bigelow, C., editor), National Technical Information Service, Springfield, Virginia 22161, USA, (1996) pp. 129-146 [5] Bray, G.H., Bucci, R.J., Colvin E.L., and Kulak, M., ASTM STP 1298, (Van Der Sluys, W.A., Piascik, R.S., and Zawierucha, R., editors), American Society for Testing and Materials, (1997) pp. 89-103 [6] Zamber, J.E. and Hillberry, B.M. (1999). Probabilistic approach to predicting fatigue lives of corroded 2024-T3. AIAA Journal, 37, 1311-1317 [7] Chubb, J.P., Morad, T.A., Hockenhull, B

Open access

Alexander Bogdanovich, Oleg Yelovoy, Leonid Sosnovskiy, Victor Komissarov and Sergey Tyurin

. Sosnovskiy L.A., Bogdanovich A.V., Yelovoy O.M., Tyurin S.A., Komissarov V.V., Sherbakov S.S. (2014), Methods and main results of Tribo-Fatigue tests, International Journal of Fatigue , 66, 207-219. 6. Sosnovskiy L.A., Shcharbakou S.S. (2005), Troppy Phenomenon, Proceedings of the World Tribology Congress , Washington. 7. Tyurin S.A., Sherbakov S.S. (2005), Experimental study of residual wave-like damage initiated by initial distortion of specimen form, Vestnik of BelSUT , 2, 88–93 (in Russian). 8. Yung-Li L., Jwo P., Hathaway R.B., Barkey M

Open access

Józef Brzęczek, Henryk Gruszecki, Leszek Pieróg, Franciszek Deszcz and Janusz Pietruszka

REFERENCES 1. J. Pietruszka “Full-Scale Fatigue Tests of PZL M28 05 SKYTRUCK Aircraft”. Transactions of Institute of Aviation , 1/2009 (196). Warsaw, 2009. 2. “Fatigue, Fail-Safe, and Damage Tolerance Evaluation of Metallic Structure for Normal, Utility, Acrobatic, and Commuter Category Airplanes”. AC 23-13A. FAA. September 29, 2005.

Open access

Józef Brzęczek, Jerzy Chodur and Janusz Pietruszka

REFERENCES 1. J. Pietruszka “Full-Scale Fatigue Tests of PZL M28 05 SKYTRUCK Aircraft”. Transactions of the Institute of Aviation , 1/2009 (196). Warsaw, 2009. 2. J. Brzęczek, H. Gruszecki, L. Pieróg, J. Pietruszka “Selected Aspects Related to Preparation of a Fatigue Test Plan of a Metallic Airframe”. Fatigue of Aircraft Structures , Issue 2014, Institute of Aviation. Warsaw, 2015. 3. J. Pietruszka „Fatigue Test of Full Scale Braced Wing and Wing Carry-Through Structure of a Commuter Aircraft” in A. Niepokólczycki ed. “Review of Aeronautical