Reconfiguration of the standard instrument departure and standard arrival routes at certain airports can bring significant reductions in fuel consumption and level of noise. This can be done either by implementing modern...
The paper aims to demonstrate the capability of LPD – Layer Plastic Deposition 3D printing technique to build complex structures for special purposes such us impregnation with carbon materials. It proposes to push the li...
In this paper the optimization of kinematics, which has great influence in performance of flapping foil propulsion, is investigated. The purpose of optimization is to design a flapping-wing micro aircraft with appropriat...
For the flow past an impervious cylinder embedded in a fluid saturated porous medium only the linear (Darcy and Darcy - Brinkman) models were used. In this work, the flow past an impermeable cylinder embedded in a fluid...
In accordance with Air Force requirements, the comparative analysis of short/medium transport aircraft comes to sustain procurement decision of short/medium transport aircraft. This paper presents, in short, the principl...
EP ID EP86134
DOI 10.13111/2066-8201.2011.3.S4
Views 106
Downloads 0
How To Cite
Horia DUMITRESCU (2011). Professor Ion Stroescu and the boundary layer: a precursor of the flow control. INCAS BULLETIN, 3(0),
37-44. https://europub.co.uk/articles/-A-86134
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Reducing Fuel Consumption in Bucharest Terminal Area for Flights Using a Standard Instrument Departure
Reconfiguration of the standard instrument departure and standard arrival routes at certain airports can bring significant reductions in fuel consumption and level of noise. This can be done either by implementing modern...
3D Complex Structures through Layer Plastic Deposition Designed for Carbon Material Impregnation
The paper aims to demonstrate the capability of LPD – Layer Plastic Deposition 3D printing technique to build complex structures for special purposes such us impregnation with carbon materials. It proposes to push the li...
Optimization of flapping-wing micro aircrafts based on the kinematic parameters using genetic algorithm method
In this paper the optimization of kinematics, which has great influence in performance of flapping foil propulsion, is investigated. The purpose of optimization is to design a flapping-wing micro aircraft with appropriat...
Brinkman–Forchheimer-Darcy flow past an impermeable cylinder embedded in a porous medium
For the flow past an impervious cylinder embedded in a fluid saturated porous medium only the linear (Darcy and Darcy - Brinkman) models were used. In this work, the flow past an impermeable cylinder embedded in a fluid...
COMPARATIVE ANALYSIS OF TRANSPORT AIRCRAFT, BACKROUND FOR SHORT/ MEDIUM COURIER TRANSPORT AIRCRAFT PROCUREMENT
In accordance with Air Force requirements, the comparative analysis of short/medium transport aircraft comes to sustain procurement decision of short/medium transport aircraft. This paper presents, in short, the principl...