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CFD Calculation of the Wing with High-lift Devices
This article deals with the CFD calculation of the initial configuration of an airliner wing equipped with double slotted flap and modified leading edge (Fixed Droop Nose + Double Slotted Flap). No slat on the leading edge ...
JU - Aeronautika, aerodynamika, letadla
- 2010 •
- Jx
Rok uplatnění
Jx - Nezařazeno - Článek v odborném periodiku (Jimp, Jsc a Jost)
Comparison of CFD Methods Applied on Vilik Flying Model
One of the tasks of the research project was to perform complete aerodynamic analysis on radio control model Vilik. For these purposes, extensive wind tunnel tests and computations with usage of panel and CFD methods have been perfo...
JU - Aeronautika, aerodynamika, letadla
- 2010 •
- Jx
Rok uplatnění
Jx - Nezařazeno - Článek v odborném periodiku (Jimp, Jsc a Jost)
Comparison of Selected CFD Methods for the calculation of Aerodynamic Characteristics of the MS 0313 and MS 0317 Airfoils
, FLUENT and EDGE represent the programs used for the computation. These CFD programs use three different computational methods. XFOIL is based on panel methods, MSES is based on Euler equations and FLUENT and ...
JU - Aeronautika, aerodynamika, letadla
- 2006 •
- D
Rok uplatnění
D - Stať ve sborníku
tabCL
Software for results displaying of high lift mechanization CFD computation.
JU - Aeronautika, aerodynamika, letadla
- 2012 •
- R •
- Link
Rok uplatnění
R - Software
Výsledek na webu
COMPARISON OF AXIAL FAN ROTOR EXPERIMENTAL DATA WITH CFD SIMULATION
Data obtained from an experimental simulation on a new test rig for axial fans are compared to a CFD simulation. The Edge solver is used and the development needed for the simulation (boundary conditions, free stream consistency) is...
JU - Aeronautika, aerodynamika, letadla
- 2016 •
- Jx •
- Link
Rok uplatnění
Jx - Nezařazeno - Článek v odborném periodiku (Jimp, Jsc a Jost)
Výsledek na webu
MatPlot
Software for displaying of computational mesh and result of CFD in FFA format.
JU - Aeronautika, aerodynamika, letadla
- 2012 •
- R •
- Link
Rok uplatnění
R - Software
Výsledek na webu
Comparison of the numerical method for calculation of the aerodynamic characteristic of the airfoils
for comparison: XFOIL, MSES, EDGE and FLUENT. Panel method (XFOIL) was compared with the solvingof the Euler (MSES) and Navier-Stokes equations (EDGE, FLUENT). Models of these methods. Numerical calculations were ...
JU - Aeronautika, aerodynamika, letadla
- 2006 •
- D
Rok uplatnění
D - Stať ve sborníku
Comm4CFD
Comm4CFD software is created and used for external communication with a CFD solver. It is focused on the prescription of aeroelastic deformation based on modal analysis. The software expands the existing CFD software capabilities, i...
Aerospace engineering
- 2017 •
- R •
- Link
Rok uplatnění
R - Software
Výsledek na webu
CFD Simulation of the Nonstationary Compressible Flow with one Degree of Freedom
The goal of this work is to present the first results of the numerical simulation of nonstationary compressible subsonic flow with one degree of freedom. We modell the flow around a 2D profil (NACA 0012) fixed in the reference point in the distance 4...
BA - Obecná matematika
- 2012 •
- D
Rok uplatnění
D - Stať ve sborníku
Wind Tunel Test of Unconventional Flying Wing Model
Article describes activity concerning unconventional flying wing model wind tunnel testing in VZLU. It was designed as a composite model, using six-component strain-gauge balance. Experimental test took place in 3m LSWT in VZLU. Results were compared...
JU - Aeronautika, aerodynamika, letadla
- 2010 •
- Jx
Rok uplatnění
Jx - Nezařazeno - Článek v odborném periodiku (Jimp, Jsc a Jost)
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