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Article
2020
Open Access
File
16 Downloads (Pure)
2019

Modelling wing wake and tail aerodynamics of a flapping-wing micro aerial vehicle

Armanini, S. F., Caetano, J. V., de Visser, C. C., Pavel, M. D., de Croon, G. C. H. E. & Mulder, M., 5 Mar 2019, In : International Journal of Micro Air Vehicles. 11, 24 p.

Research output: Contribution to journalArticleScientificpeer-review

Open Access
File
2 Citations (Scopus)
98 Downloads (Pure)
2018

Helicopter Roll-Axis Instabilities induced by Pilot Cyclic Control: A Physical Explanation

Pavel, M. & Ionita, A., 2018, In : INCAS Bulletin. 10, 3, p. 139-156 18 p.

Research output: Contribution to journalArticleScientificpeer-review

Open Access
File
22 Downloads (Pure)

Instability mechanism of roll/Lateral biodynamic rotorcraft–Pilot couplings

Muscarello, V., Masarati, P., Quaranta, G., Tod, G., Gomand, J., Malburet, F. & Pavel, M. D., 1 Apr 2018, In : Journal of the American Helicopter Society. 63, 2, 13 p., 022004.

Research output: Contribution to journalArticleScientificpeer-review

Nitros: An innovative training program to enhance rotorcraft safety

Quaranta, G., Pavel, M., Barakos, G., White, M. & Mulder, M., 2018, In : Annual Forum Proceedings - AHS International. 2018-May, 14 p.

Research output: Contribution to journalArticleScientificpeer-review

Open Access
File
16 Downloads (Pure)
2017
Open Access
File
1 Citation (Scopus)
15 Downloads (Pure)
2016

Designing the Ornicopter, a tailless helicopter with active flapping blades: a case study

Wan, J. & Pavel, M., 2016, In : Journal of Aerospace Engineering. 230, 12, p. 2195-2219 25 p.

Research output: Contribution to journalArticleScientificpeer-review

Open Access
File
70 Downloads (Pure)

Understanding pilot biodynamical feedthrough coupling in helicopter adverse roll axis instability via lateral cyclic feedback control

Tod, G., Pavel, M., Malburet, F., Gomand, J. & Barre, PJ., 2016, In : Aerospace Science and Technology. 59, p. 18–31

Research output: Contribution to journalArticleScientificpeer-review

Open Access
File
3 Citations (Scopus)
14 Downloads (Pure)
2015

Practises to identify and prevent adverse aircraft-and-rotorcraft-pilot couplings: A design perspective

Pavel, MD., Masarati, P., Gennaretti, M., Jump, M., Zaichik, L., Dang-Vu, B., Lu, L., Yilmaz, D., Quaranta, G., Ionita, A. & Serafini, J., 2015, In : Progress in Aerospace Sciences. 76, p. 55-89 35 p.

Research output: Contribution to journalArticleScientificpeer-review

Open Access
21 Citations (Scopus)

Practises to identify and prevent adverse aircraft-and-rotorcraft-pilot couplings: A ground simulator perspective

Pavel, MD., Jump, M., Masarati, P., Zaichik, L., Dang-Vu, B., Smaili, H., Quaranta, G., Stroosma, O., Yilmaz, D., Johnes, M., Gennaretti, M. & Ionita, A., 2015, In : Progress in Aerospace Sciences. 77, p. 54-87 34 p.

Research output: Contribution to journalArticleScientificpeer-review

Open Access
12 Citations (Scopus)
2014

State-Space Rotor Aerolastic Modeling for Real-Time Helicopter Flight Simulation

Gori, R., Pausilli, F., Pavel, MD. & Gennaretti, M., 2014, In : Advanced Materials Research. 1016, p. 451-459 9 p.

Research output: Contribution to journalArticleScientificpeer-review

12 Citations (Scopus)

The Ornicopter - a tailless helicopter with active flapping blades

Wan, J. & Pavel, MD., 2014, In : The Aeronautical Journal. 118, 1205, p. 743-773 31 p.

Research output: Contribution to journalArticleScientificpeer-review

2 Citations (Scopus)
2013

Adverse rotorcraft pilot couplings¿Past, present and future challenges

Pavel, MD., Jump, M., Vu, BD., Masarati, P., Ionita, A., Zaichik, L., Smaili, H., Quaranta, G., Yilmaz, D., Jones, M., Serafini, J. & Malecki, J., 2013, In : Progress in Aerospace Sciences. 62, p. 1-51 51 p.

Research output: Contribution to journalArticleScientificpeer-review

Open Access
52 Citations (Scopus)

An acceleration measurements-based approach for helicopter nonlinear flight control using Incremental Nonlinear Dynamic Inversion

Simplicio, P., Pavel, MD., van Kampen, E. & Chu, QP., 2013, In : Control Engineering Practice. 21, 8, p. 1065-1077 13 p.

Research output: Contribution to journalArticleScientificpeer-review

87 Citations (Scopus)

A Practical Biodynamic Feedthrough Model for Helicopters

Venrooij, J., Pavel, MD., Mulder, M., van der Helm, FCT. & Bulthoff, HH., 2013, In : CEAS Aeronautical Journal. 2013/TBD, p. 421-432 12 p.

Research output: Contribution to journalArticleScientificpeer-review

Validation of mathematical models for helicopter flight simulators - Past, Present and Future Challenges

Pavel, MD., White, M., Padfield, GD., Roth, G., Hamers, M. & Taghizad, A., 2013, In : The Aeronautical Journal. 117, no. 1190, p. 343-388 46 p.

Research output: Contribution to journalArticleScientificpeer-review

11 Citations (Scopus)
2012

Concept of a predictive tool for ship-helicopter operational limitations of various in-service conditions

Hoencamp, A. & Pavel, MD., 2012, In : American Helicopter Society. Journal. 57, 3, p. 1-9 9 p.

Research output: Contribution to journalArticleScientificpeer-review

9 Citations (Scopus)

Validation of the Beddoes-Leishman dynamic stall model for horizontal axis wind turbines using Mexico data

Balbino Dos Santos Pereira, R., Schepers, JG. & Pavel, MD., 2012, In : Wind Energy.

Research output: Contribution to journalArticleScientificpeer-review

Open Access
32 Citations (Scopus)
2010

Investigation of Chinook helicopter operations with an external slung load after cable failure

Pavel, MD., 2010, In : The Aeronautical Journal. 114, 1156, p. 345-365 21 p.

Research output: Contribution to journalArticleScientificpeer-review

2009

Optimization of Rotorcraft Simultaneous Noninterfering Noise Abatement Approach Procedures

Visser, HG., Pavel, MD. & Tang, SF., 2009, In : Journal of Aircraft: devoted to aeronautical science and technology. 46, 6, p. 2156-2161 6 p.

Research output: Contribution to journalArticleScientificpeer-review

5 Citations (Scopus)
2008

Prediction of the necessary degrees of freedom for helicpter real-time simulation models

Pavel, MD., 2008, In : Journal of Aircraft: devoted to aeronautical science and technology. 45, 4, p. 1256-1266 11 p.

Research output: Contribution to journalArticleScientificpeer-review

1 Citation (Scopus)
2006

The extension of ADS-33-metrics for agility enhancement and structural load alleviation

Pavel, MD. & Padfield, GD., 2006, In : American Helicopter Society. Journal. 51, 4, p. 319-330 12 p.

Research output: Contribution to journalArticleScientificpeer-review

6 Citations (Scopus)
2002

On the question of adequate modelling of steady-state rotor disc-tilt for helicopter manoeuvring flight

van Aalst, R. & Pavel, MD., 2002, In : European Journal of Operational Research. p. 1-8 8 p.

Research output: Contribution to journalArticleScientificpeer-review