Miguel Silvestre

Dr. Miguel Silvestre

Universidade da Beira Interior
+1
orcid

Research Focus & Metrics

Academic Career Length

22Years (2005-Present)

(Calculated once Scilit publication data is synced: current year − year of first publication + 1)

Representative Publications

View All Publications
1 May 2016 in Aerospace Science and Technology
Verified
Journal Article
Closed access
JMJ. Morgado
J. Morgado
RVR. Vizinho
R. Vizinho
Miguel SilvestreMiguel Silvestre
Miguel Silvestre
Jose PascoaJose Pascoa
Jose Pascoa

1 December 2013 in Journal of Wind Engineering and Industrial Aerodynamics
Verified
Journal Article
Closed access
JMJoão P. Monteiro
João P. Monteiro
Miguel SilvestreMiguel Silvestre
Miguel Silvestre
HPHugh Piggott
Hugh Piggott
JAJorge C. André
Jorge C. André

1 September 2015 in Aerospace Science and Technology
Verified
Journal Article
Closed access
JMJ. Morgado
J. Morgado
MAM. Abdollahzadeh
M. Abdollahzadeh
Miguel SilvestreMiguel Silvestre
Miguel Silvestre
Jose PascoaJose Pascoa
Jose Pascoa

1 January 2015 in Journal of Propulsion and Power
Verified
Journal Article
Closed access
JMJ. Morgado
J. Morgado
Miguel SilvestreMiguel Silvestre
Miguel Silvestre
Jose PascoaJose Pascoa
Jose Pascoa
This paper reports the development of a new propeller design and analysis tool. JBLADE uses an improved version of blade element momentum that embeds a new model for the three-dimensional flow equilibrium. In addition, a new method for the prediction of the airfoil drag coefficient at a 90 deg angle of attack for a better poststall modeling is also presented. The software is developed as an open-source tool for the simulation of propellers and has the capability to estimate the performance of a given propeller geometry in design and offdesign operating conditions. The software allows the introduction of the blade geometry as an arbitrary number of sections. To validate the code, the propellers from NACA Technical Report 530 by Gray (“Wind-Tunnel Tests of Two Hamilton Standard Propellers Embodying Clark Y and NACA 16-Series Blade Sections,” 1941) and NACA Technical Report 594 by Theodorsen et al. (“Characteristics of Six Propellers Including the High-Speed Range,” 1937) were simulated and the results were ...

1 December 2013 in Engineering Failure Analysis
Verified
Journal Article
Closed access
VIVirgínia Infante
Virgínia Infante
JSJ.M. Silva
J.M. Silva
Miguel SilvestreMiguel Silvestre
Miguel Silvestre
RBRicardo Baptista
Ricardo Baptista

11 August 2020 in Energies
Verified
Journal Article
Open access
PDF file
PAPedro Alves
Pedro Alves
Miguel SilvestreMiguel Silvestre
Miguel Silvestre
PGPedro Gamboa
Pedro Gamboa
The race for speed ruled the early Jet Age on aviation. Aircraft manufacturers chased faster and faster planes in a fight for pride and capability. In the early 1970s, dreams were that the future would be supersonic, but fuel economy and unacceptable noise levels made that era never happen. After the 1973 oil crisis, the paradigm changed. The average cruise speed on newly developed aircraft started to decrease in exchange for improvements in many other performance parameters. At the same pace, the airliner’s power-plants are evolving to look more like a ducted turboprop, and less like a pure jet engine as the pursuit for the higher bypass ratios continues. However, since the birth of jet aircraft, the propeller-driven plane has lost its dominant place, associated with the idea that going back to propeller-driven airplanes, and what it represents in terms of modernity and security, has started a propeller avoidance phenomenon with travelers and thus with airlines. Today, even with the modest research effort since the 1980s, advanced propellers are getting efficiencies closer to jet-powered engines at their contemporary typical cruise speeds. This paper gives a brief overview of the performance trends in aviation since the last century. Comparison examples between aircraft designed on different paradigms are presented. The use of propellers as a reborn propulsive device is discussed.