Zobrazeno 1 - 10
of 96
pro vyhledávání: '"Boško Rašuo"'
Publikováno v:
Aerospace, Vol 11, Iss 1, p 26 (2023)
In the present work, the potential application of machine learning techniques in the flutter prediction of composite materials missile fins is investigated. The flutter velocity data set required for different fin aerodynamic geometries and materials
Externí odkaz:
https://doaj.org/article/4abbc53ccaca49c3b0c02a948c8bbd42
Publikováno v:
Aerospace, Vol 8, Iss 10, p 275 (2021)
Published results for standard wind tunnel models at non-standard test conditions are quite rare and/or may not be available. It has been found that those results are a useful aid in preparations for a number of wind tunnel tests in the Military Tech
Externí odkaz:
https://doaj.org/article/23a8cd1ae8014e8cb4c36c24b7f6b311
Publikováno v:
FME Transactions. 51:117-130
Automatic Dependent Surveillance-Broadcast (ADS-B) is a multiparameter surveillance system designed to improve key segments of air traffic: enabling real-time surveillance, raising safety and efficiency levels, and improving flight information and we
Publikováno v:
FME Transactions. 50:576-585
In the present work, the aeroelastic stability of tapered composite plates is investigated. Existing flutter models, based on the typical section approach, are reviewed for quasi-steady and unsteady low Mach number axial flows and modified for the th
Publikováno v:
FME Transactions. 50:732-744
In the present paper, the dynamic and static stability of composite shells for different aerodynamic configurations is investigated. Based on the existing models for flutter and torsional divergence, modified to include material anisotropy, stability
Autor:
Nebojša Ćurčić, Novak Milošević, Marina Stamenović, Marta Trninić, Boško Rašuo, Mirko Dinulović
Publikováno v:
FME Transactions, Vol 49, Iss 2, Pp 308-314 (2021)
Noise is becoming one of the problems in many industrial applications. In this paper the aerodynamic noise in air duct system that arises from air flow passing over a surface of turning vanes is investigated. Based on Proudman's formula using Lighthi
Autor:
Branimir Krstic, A Younes Djemaoune, D Marjan Dodic, P Boško Rašuo, P Stefan Rašić, R Daniel Radulović
Publikováno v:
FME Transactions, Vol 49, Iss 4, Pp 969-976 (2021)
Honeycomb sandwich structures, composed of many regularly arranged hexagonal cores and two skins, show excellent impact performance due to strong energy absorption capability under impact loads. In this paper, a numerical study of low velocity impact
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. 235:1129-1145
The goal of this work is to build a unique numerical method to obtain the basic aerodynamic characteristics of the aircraft and to enable a wide application of the method in the analysis of some aerodynamic characteristics of the aircraft, without us
Autor:
Katarina Maksimovic, Gordana Kastratović, Aleksandar Grbović, Boško Rašuo, Mirjana Puharić, Nenad Vidanović
Publikováno v:
Journal of Spacecraft and Rockets
The main goal of this paper is to expand previously conducted study and consequently to upgrade the proposed multimodular numerical framework developed for fluid–structure interaction simulation (FSI) and multidisciplinary design optimization (MDO)
Publikováno v:
Tehnika. 75:457-466
In this work complete methodology for calculation and analysis of fluid flow in air ducts is presented. In order to minimize outlet pressure drop and to reduce the duct vibrations the plates with airfoil cross sections are added to duct critical zone