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Review of flow-control devices for wind-turbine performance enhancement
It is projected that, in the following years, the wind-energy industry will maintain its rapid
growth over the last few decades. Such growth in the industry has been accompanied by the …
growth over the last few decades. Such growth in the industry has been accompanied by the …
A synergistic glance at the prospects of distributed propulsion technology and the electric aircraft concept for future unmanned air vehicles and commercial/military …
AS Gohardani - Progress in Aerospace Sciences, 2013 - Elsevier
Distributed propulsion is one of the revolutionary candidates for future aircraft propulsion. In
this journal article, the potential role of distributed propulsion technology in future aviation is …
this journal article, the potential role of distributed propulsion technology in future aviation is …
[KÖNYV][B] Neurotechnology for biomimetic robots
J Ayers, JL Davis, A Rudolph - 2002 - books.google.com
An overview of neurotechnology, the engineering of robots based on animals and animal
behavior. The goal of neurotechnology is to confer the performance advantages of animal …
behavior. The goal of neurotechnology is to confer the performance advantages of animal …
Active load control techniques for wind turbines.
CP Van Dam, DE Berg, SJ Johnson - 2008 - osti.gov
This report provides an overview on the current state of wind turbine control and introduces
a number of active techniques that could be potentially used for control of wind turbine …
a number of active techniques that could be potentially used for control of wind turbine …
Numerical studies of the effects of active and passive circulation enhancement concepts on wind turbine performance
C Tongchitpakdee, S Benjanirat, LN Sankar - 2006 - asmedigitalcollection.asme.org
The aerodynamic performance of a wind turbine rotor equipped with circulation
enhancement technology (trailing-edge blowing or Gurney flaps) is investigated using a …
enhancement technology (trailing-edge blowing or Gurney flaps) is investigated using a …
Numerical simulations of the steady and unsteady aerodynamic characteristics of a circulation control wing airfoil
Y Liu, L Sankar, R Englar, K Ahuja - 39th Aerospace Sciences Meeting …, 2001 - arc.aiaa.org
The aerodynamic characteristics of a Circulation Control Wing (CCW) airfoil have been
numerically investigated, and comparisons with experimental data have been made. The …
numerically investigated, and comparisons with experimental data have been made. The …
Numerical simulation on plasma circulation control airfoil
PF Zhang, B Yan, AB Liu, JJ Wang - AIAA journal, 2010 - arc.aiaa.org
CIRCULATION control (CC) concept is inspired by the well known Coanda effect, invented
by Romanian inventor Henri Coanda in early 1930s [1]. It means the tendency offluids to …
by Romanian inventor Henri Coanda in early 1930s [1]. It means the tendency offluids to …
Lift enhancement method by synthetic jet circulation control
PF Zhang, B Yan, CF Dai - Science China Technological Sciences, 2012 - Springer
A novel circulation control technique is proposed to overcome the shortcomings of blowing
jet circulation control, which uses the synthetic jet as the actuator and avoids the limitation …
jet circulation control, which uses the synthetic jet as the actuator and avoids the limitation …
A numerical investigation into the effect of engine bleed on performance of a single-spool turbojet engine
NU Rahman, JF Whidborne - Proceedings of the Institution of …, 2008 - journals.sagepub.com
A real time simulation model has been developed to investigate the effect of variable engine
bleed on steady state and transient performance of a single-spool turbojet engine. The …
bleed on steady state and transient performance of a single-spool turbojet engine. The …
Assessment of leading-edge devices for stall delay on an airfoil with active circulation control
M Burnazzi, R Radespiel - CEAS Aeronautical Journal, 2014 - Springer
The use of active, internally blown high-lift flaps causes the reduction of the stall angle of
attack, because of the strong suction peak generated at the leading-edge. This problem is …
attack, because of the strong suction peak generated at the leading-edge. This problem is …