An online distributed algorithm for inferring policy routing configurations [PDF]
, 2016 We present an online distributed algorithm, the Causation Logging Algorithm (CLA), in which Autonomous Systems (ASes) in the Internet individually report route oscillations/flaps they experience to a central Internet Routing Registry (IRR).
Epstein, Samuel Randall
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Proposal for an Enhanced Monitoring Technique for Active Control of Aircraft Flap Asymmetry
Engineering ProceedingsThis paper presents an innovative active monitoring strategy to manage asymmetry in aircraft flaps. Complex mechanical systems like high-lift devices may undergo a wide range of faults, such as a broken transmission torsion bar or wear and tear on ...
Leonardo Baldo +2 more
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Indian Journal of Plastic Surgery, 2019 Introduction Breast conservation therapy (BCT) and oncoplastic breast surgery (OBS) are now established modalities of treatment for breast cancer, with proven oncological safety.
Dushyant Jaiswal +3 more
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The aerodynamic characteristics of a model wing having a split flap deflected downward and moved to the rear [PDF]
Tests were made on a model wing with three different sized split trailing-edged flaps, in the NACA 7 by 10 foot wind tunnel. The flaps were formed of the lower rear portion of the wing and were rotated downward about axes at their front edges.
Harris, Thomas E, Weick, Fred E
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Elastocapillary folding of three dimensional micro-structures using water pumped through the wafer via a silicon nitride tube [PDF]
, 2011 In this paper we present the first investigation of a batch method for folding of threedimensional micrometer-sized silicon nitride structures by capillary forces.
Abelmann, L. +5 more
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Indian Journal of Dentistry, 2014 For full-thickness lip defects, the choice of reconstructive option depends on the size of the defect. Defects of one-quarter to one-third of the upper lip can be closed primarily. Largerdefects measuring one-third to two-thirds of the lower lip width may be closed with the Karapandzic, Abbe or Estlander flaps.
Khan, Abdul Ahad Ghaffar +1 more
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Modelling flexible thrust performance for trajectory prediction applications in ATM [PDF]
, 2016 Reduced thrust operations are of widespread use nowadays due to their inherit benefits for engine conservation. Therefore, in order to enable realistic simulation of air traffic management (ATM) scenarios for purposes such as
Casado, Enrique +7 more
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Enhancing Stability through Experimental Research on the Flapped Horizontal Axial Wind Turbine
Mağallaẗ Al-kūfaẗ Al-handasiyyaẗThis study examines the effects of changing flap angles on the aerodynamic performance of a wind turbine blade, concentrating on torque coefficient (Cm), thrust coefficient (Ct), power coefficient (Cp), and power in watts over a range of rotational ...
Qassim Wanis . M +2 more
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A passive gust alleviation system for a light aircraft [PDF]
A passive aeromechanical gust alleviation system was examined for application to a Cessna 172. The system employs small auxiliary wings to sense changes in angle of attack and to drive the wing flaps to compensate the resulting incremental lift.
Harlan, R. B., Roesch, P.
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Aerodynamic Characteristics at a Mach Number of 6.8 of Two Hypersonic Missile Configurations, One with Low-Aspect-Ratio Cruciform Fins and Trailing-Edge Flaps and One with a Flared Afterbody and All-Movable Controls [PDF]
, 1958 An investigation has been made to determine the aerodynamic characteristics in pitch at a Mach number of 6.8 of hypersonic missile configurations with cruciform trailing-edge flaps and with all-movable control surfaces.
Bernot, P. T., Robinson, R. B.
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