Maderuelo, C. and Climent, H. CASA DT-89-3220. Validación de un Método Analítico para el Cálculo de Cargas de Rodadura, July 1990.
Pérez-Galán, J.L., Portas, J.A., Chorro, J.M., López-Arévalo, J.L. and Climent, H., Aircraft Taxi Loads Full Scale Tests and Correlation with Numerical Simulations. International Forum of Aeroelasticity and Structural Dynamics 2001. Madrid, Spain, 5-7 June 2001.
Beltrán, F. and Martí, J. Análisis de Impactos de pájaro en Bordes de Ataque Informe a Construcciones Aeronáuticas S.A. por Principia. Informes 275 (CASA-3000; 26 July 1994) y 280 (Airbus A330/A340; 31-Oct-1994).
Martinez, F., Rico, G., Franganillo, A. and Climent, H., Bird Impact on an Aircraft Leading Edge. ABAQUS User’s Conference, Paris, France, 31 May – 2 June 1994, pp 565–577.
Pérez Galán, J.L., Climent, H. and Le PAGE, F.
Non-linear Response of Metallic and Composite Aeronautical Fuselage Structures under Crash Loads and Comparison with Full Scale Test. European Congress on Computational Methods in Applied Sciences and Engineering ECCOMAS 2000, Barcelona, Spain, 11-14 September 2000.
Wigenraad, J.F.M., Santoro, D., Le Page, F., Kindervater, C. and Climent, H.
Development of a Crashworthy Composite Fuselage Concept for a Commuter Aircraft 57th Annual Forum of the American Helicopter Society, Washington DC, USA, 9-11 May 2001.
Palacios, R., Climent, H., Karlsson, A. and Winzell, B.
Assessment of Strategies for Correcting Linear Unsteady Aerodynamics using CFD or Test Results. International Forum of Aeroelasticity and Structural Dynamics 2001. Madrid, Spain, 5-7 June, 2001.
Oliver, M., Climent, H. and Rosich, F.
Non-linear Effects of Applied Loads and Large Deformations on Aircraft Normal Modes. RTO Meeting Proceedings 36. Structural Aspects of Flexible aircraft Control. Chapter 21. Papers presented at the Specialists’ Meeting of the RTO Applied Vehicle Technology Panel (AVT) held in Otawa, Canada, 18-20 October 1999.
Oliver, M., Rodriguez Ahlquist, J., Martinez Carreño, J. AND Climent, H.
A400M GVT: the challenge of nonlinear modes in very large GVT’s. International Forum of Aeroelasticity and Structural Dynamics 2009, Seattle, USA, 20-25 June 2009.
Gerardi, A.G. and Lohwasser, A.K.
Computer Program for the Prediction of Aircraft Response to Runway Roughness, AFWL-TR-73-109, Volume I and II, Air Force Weapons Laboratory, Kirtland AFB, New Mexico, USA, September 1973.
Petiau, C. and Celier, A.
Methode de Simulation Numerique du Systeme Avion Atterriseur, AGARD-CP-326. Aircraft Dynamic Response to Damaged and Repaired Runways Brussels, Belgium, 4-9 April 1983.
Portas, J.A., Pérez Galán, J.L. and Climent, H. CASA NT-5-ADD-00005. C295M Flight Test Results for Operation on Uneven and Unpaved Runways. January 2001.
Bisplinghoff, R.L., Ashley, H. and Halfman, R.L.
Aeroelasticity, Addison-Wesley Publishing Co, 1955.
Mcpherson, A.E., Evans, J. Jr and Levy, S. Influence of Wing Flexibility on Force-Time Relation in Shock Strut Following Vertical Landing Impact, NACA TN 1995, November 1949.
Maderuelo, C., Pérez Galán, J.L., Claverías, S., Climent, H. and Rendueles, B.
Flight Test Validation of a Fully Coupled Flexible Landing Gear and Flexible Aircraft Modes. International Forum of Aeroelasticity and Structural Dynamics 2005, Munich, Germany, 28 June – 1 July 2005.
Ramos, J. and Kamoulakos, A. ESI Report describing Development of SPH/Lagrangian Bird Model, CRAVHI Deliverable D1.4.2. October 2002.
Pérez-Galán, J.L. and Climent, H. EADS-CASA, Final Report on HTP Stochastic Impact/Crash Simulation using ST-ORM with Monte Carlo Simulation Method, CRAVHI Deliverable D3.3.1 February 2004.
Pérez-Galán, J.L., Strömberg, A.M. and Climent, H.
Stochastic Approach to Bird Strike Numerical Simulation. International Forum of Aeroelasticity and Structural Dynamics 2005. Munich, Germany. 28 June – 1 July 2005.
Beltrán, F., Rueda, F. and Climent, H. EADS-CASA NT-J-ADD-01006, EF-2000. Production A/C. Bird strike analysis of wing slats, July 2001.
Ibáñez, P., Benítez, L. and Climent, H. EADS-CASA NT-A4-AA0-08004, A400M: Bird impact on the HTP leading edge. Numerical simulations, sensitivity analyses and suggested structural improvements, June 2008.
Benítez, L., Pérez-Galán, J.L. and Climent, H. EADS-CASA NT-A4-AA0-07016 issue B, A400M: Bird Impact on the Nacelle Centre Upper Cowl. Deterministic and Stochastic Numerical Simulations, August 2008.
Pérez-Galán, J.L. and Climent, H. EADS-CASA, Assessment Report on the use of Stochastic Techniques for HVI Simulations applied to complex metallic and composite aeronautical structures, CRAHVI deliverable D.6.1.2, April 2004.
Rueda, F., Correal, A., De Castro, A., Benitez, L. and Climent, H.
A new Approach for the Wheels-Up Landing Analysis and Certification of the A400M, EuroPAM 2008. The 17th European Conference and Exhibition on Simulation-Based Design, Prague, Czech Republic, 29-30 May 2008.
Benitez, L., Climent, H., Rueda, F. and Ibáñez, P.
New approach for Crashworthiness of Aircraft Wheels Up Landing. 6th International KRASH User’s Seminar (IKUS6), Stuttgart, Germany. 15-17 June 2009.
Benitez, L., Climent, H., Rueda, F. and Pérez de la Serna, A.
Impact Loads in Aircraft Wheels Up Landing. International Forum of Aeroelasticity and Structural Dynamics 2009, Seattle, USA. 20-25 June 2009.
Climent, H., Benitez, L., Rosich, F., Rueda, F. and Pentecote, N.
Aircraft Ditching Numerical Simulation. 25th Congress of International Council of the aeronautical Sciences ICAS 2006. Hamburg, Germany, 3-8 September 2006.
Wernsdorfer, T., Keller, K. and Climent, H. EADS-CASA NT-3-AA0-04004, CN-235-300M Deepwater Ditching Tests Evaluation Report, March 2005.
Pentecote, N. Validation of PAM-CRASH code for the simulation of the impact on water, DLR – IB 435.2003/3, January 2003.
Triviño, V., Pérez-Galán, J.L. and Climent, H.
Ice impacts on Aeronautical Structures, International Forum of Aeroelasticity and Structural Dynamics 2007, Stockholm, Sweden, 18 – 20 June 2007.
Benítez, L. and Climent, H. EADS-CASA NT-T-AA0-07005 Parametric Vulnerability Studies of Fluid Filled CFRP Structures, April 2007.