[PDF][PDF] Aerodynamic characteristics of airfoil with single slotted flap for Light Airplane Wing
M Todorov - Proc. of AFASES, 2015 - academia.edu
A numerical study was performed on a NACA 23012 airfoil with a single slotted flap to
examine the aerodynamic coefficients at Reynolds number of 3× 106, and for help to …
examine the aerodynamic coefficients at Reynolds number of 3× 106, and for help to …
Aerodynamic characteristics of airfoil with single plain flap for light airplane wing
M Todorov - … Conference on Military Technologies (ICMT) 2015, 2015 - ieeexplore.ieee.org
A numerical study was performed on a NACA 23012 airfoil with a single plain flap to
examine the aerodynamic coefficients at Reynolds number of 3× 10 6, and to help for …
examine the aerodynamic coefficients at Reynolds number of 3× 10 6, and to help for …
[PDF][PDF] Study the influence of a gap between the wing and slotted flap over the aerodynamic characteristics of ultra-light aircraft wing airfoil
C Velkova, M Todorov, G Durand - Journal of Mechanics …, 2015 - davidpublisher.com
The purpose of the study is to assess what the influence of the distance of the gap is
between the wing and slotted flap on the aerodynamic characteristics of ultra-light aircraft …
between the wing and slotted flap on the aerodynamic characteristics of ultra-light aircraft …
RANS Simulations of the High Lift Common Research Model with open-source code SU2
A Matiz-Chicacausa, J Escobar, D Velasco… - Numerical Simulation of …, 2018 - Springer
High-lift devices have been used in aviation for several decades as an effective solution to
keep takeoff and landing speeds within an acceptable range, while increasing wing loading …
keep takeoff and landing speeds within an acceptable range, while increasing wing loading …
Comparison of Octree and Omni-Tree Cartesian grid for civil-plane high-lift model simulations
W Sang, Y Shi - Journal of aircraft, 2013 - arc.aiaa.org
This comparative study is motivated by recent developments dealing with transport aircraft
high-lift aerodynamics. Different than these developments Cartesian grids are used to …
high-lift aerodynamics. Different than these developments Cartesian grids are used to …
Alternative air brake concepts for transport aircraft steep approach
US Jung - 2012 - mediatum.ub.tum.de
Alternative Air Brake Concepts for Transport Aircraft Steep Approach Page 1 Technische
Universität München Lehrstuhl für Aerodynamik und Strömungsmechanik Alternative Air Brake …
Universität München Lehrstuhl für Aerodynamik und Strömungsmechanik Alternative Air Brake …
Viscous flow analysis of a twin-engine commercial transport aircraft in high lift landing configuration
Extensive unstructured-grid CFD analysis has been performed for predicting performance of
a twin-engine commercial transport airplane in landing configuration. The objective of the …
a twin-engine commercial transport airplane in landing configuration. The objective of the …
[PDF][PDF] Viscous Flow Analysis of a Twin-engine Commercial Transport Aircraft in High Lift Landing Configuration
Extensive unstructured-grid CFD analysis has been performed for predicting performance of
a twin-engine commercial transport airplane in landing configuration. The objective of the …
a twin-engine commercial transport airplane in landing configuration. The objective of the …
AERODYNAMIC CHARACTERISTICS OF AIRFOIL WITH SINGLE SLOTTED FLAP FOR LIGHT AIRPLANE WING.
M Damianov Todorov - … Research & Education in the Air …, 2015 - search.ebscohost.com
A numerical study was performed on a NACA 23012 airfoil with a single slotted flap to
examine the aerodynamic coefficients at Reynolds number of 3x10< sup> 6, and for help to …
examine the aerodynamic coefficients at Reynolds number of 3x10< sup> 6, and for help to …