Issue 43

P. Zampieri et alii, Frattura ed Integrità Strutturale, 43 (2018) 191-204; DOI: 10.3221/IGF-ESIS.43.15 204 [2] Federal Aviation Regulations FAR25. [3] Williams, D., Jones, R.P.N., Dynamic Loads in Aeroplanes under Given Impulsive Loads with Particular Reference to Landing and Gust Loads on a Large Flying Boat, Britain: Aeronautical Research Council; (1948) TR No. 2221. [4] McPherson, A.E., Evans, Jr. J., Levy, S., Influence of Wing Flexibility on Force-Time Relation in Shock Strut Following Vertical Landing Impact, Washington, (1949), NACA TN 1995. [5] Cook, F.E., Milwitzky, B., Effect of Interaction on Landing-Gear Behaviour and Dynamic Loads in a Flexible Airplane Structure, United States, (1956), NACA TR 1278. [6] Luber, W.G., Dill E., Kainz, K., Dynamic landing loads on combat aircraft with external stores using finite element models, in: IMAC-XXV: Conference and Exposition on Structural Dynamics, Orlando, FL (2007) 19–22. [7] Pérez, J.L., Benítez, L.H., Oliver, M., Climent, H., Survey of aircraft structural dynamics nonlinear problems and some recent solutions, Aeronaut. J. 115 (1173) (2011) 653–668. DOI: 10.1017/S0001924000006382. [8] Suresh, P., Nesar, S., Radhakrishnan, G., Dynamic landing response analysis of a flexible tailless delta wing aircraft, Int. J. Aerosp. Innov. 4 (3–4) (2012) 103–117. DOI: 10.1260/1757-2258.4.3-4.103. [9] Chester, D.H., Aircraft landing impact parametric study with emphasis on nose gear landing conditions, J. Aircr. 39 (3) (2002) 394–403. DOI: 10.2514/2.2964. [10] Lomax, T.L., Structural Loads Analysis for Commercial Aircraft: Theory and Practice, AIAA Education Series (1996). ISBN-13: 978-1563471148. [11] Infante, V., Fernandes, L., Freitas, M., Baptista, R., Failure analysis of a nose landing gear fork, Eng. Fail. Anal., 82 (2017) 554-565. DOI: 10.1016/j.engfailanal.2017.04.020. [12] Imran, M., Ahmed, R.M. S., Haneef. M., FE Analysis for Landing Gear of Test Air Craft, Mater. Today, 2 (4-5) (2015) 2170-2178. DOI: 10.1016/j.matpr.2015.07.228. [13] Redonnet, S., Ben Khelil, S., Bulté, J., Cunha, G., Numerical characterization of landing gear aeroacoustics using advanced simulation and analysis techniques, J. Sound. Vib., 403 (2017) 214-233. DOI: 10.1016/j.jsv.2017.05.012 [14] Viúdez-Moreiras, D., Martín, M., Abarca, R., Andrés, E., Ponsín, J., Monge, F., Surrogate modeling for the main landing gear doors of an airbus passenger aircraft, Aerosp. Sci. Technol., 68 (2017) 135-148. DOI: 10.1016/j.ast.2017.04.021 [15] ADAMS User Reference Manual 2015, MSC Software Corporation. [16] Hallquist, J.O., Ls-dyna theory manual (2006). ISBN 0-9778540-0-0.