Numerical Investigation of the Wing-in-Ground Effect on Aerodynamic Characteristics
Journal Title: Problemy Mechatroniki. Uzbrojenie, lotnictwo, inżynieria bezpieczeństwa - Year 2016, Vol 7, Issue 4
Abstract
This paper presents the numerical evaluation of ground (proximity) effects on the basic aerodynamic characteristics of a specifically designed airplane model. The ground effects were investigated in relation to the angle of attack and flight altitude. The results were referenced to the characteristics of an object in motion unaffected by ground effects.
Authors and Affiliations
Stanisław WRZESIEŃ, Michał FRANT, Maciej MAJCHER
Keywords
Related Articles
- EP ID EP186883
- DOI 10.5604/01.3001.0009.5022
- Views 83
- Downloads 0
Urządzenia zabezpieczająco-uzbrajające w zapalnikach
W artykule przedstawiono wymogi stawiane zapalnikowym urządzeniom zabezpieczająco-uzbrajającym w świetle obowiązujących norm. Ponadto zaprezentowano podstawowe rodzaje urządzeń przerywających łańcuch ogniowy oraz nowe te...
Relative Explosive Strength and Detonation Characteristics of Some Explosive Mixtures Containing Urea and Peroxides
Several mixtures, based on urea, urea hydrogen peroxide complex (UHP), triacetone triperoxide (TATP) with some inorganic oxidants were studied by means of ballistics mortar with TNT as a reference standard. The detonatio...
Applying AIM-9X on MiG-29 – Initial Analysis of MiG-29 Weapon System Modernizations
Author, in this article, describes technical realizability of assembly AIM-9X missile on MiG-29, gives also in the introduction information about aircraft modernizations necessity. Second and third part of the article co...
Electronic Time Modules of the Enhanced Mechanical Resistance and the Precision of Action
In the Military Institute of Armament Technology in Zielonka, Poland, the works on the improvement of the mechanical resistance and the precision of action of the artillery fuses with electronic time modules were taken u...
The Control System of the Active Magnetic Bearing in the Aircraft Nacelle Actuation
The flight control system of the modern aircrafts, i.e. Boeing 787 and Airbus A380, are designed in the “more electric aircraft” technology (MEA). This technology make an assumption of the use more electrical elements in...