Aerodynamic analysis of fighter aircraft F-16 with external stores

Download
2003
Erhan, Haluk

Suggestions

Aerodynamic analysis of external stores on aircraft
Bozkurttaş, Meliha; Kavsaoğlu, Mehmet Şerif; Department of Aeronautical Engineering (2001)
Aerodynamic investigation of a model scale helicopter rotor in ground effect
Şahbaz, Mehmet; Kurtuluş, Dilek Funda; Sezer Uzol, Nilay; Department of Aerospace Engineering (2017)
In this thesis, ground effect issue which is a vital topic for helicopter industry is investigated with model scale.For this purpose, a test setup with model helicopter rotor is established. With setup, ground effect is investigated with inclined ground and ground without inclination. Thrust and torque values are obtained for different rotation speeds with constant collective pitch. Comparison with literature is done and reliability of the test setup is proven. Inclined Ground Effect and Ground Effect with ...
Aerodynamic Design Analysis Of Missiles With Strake Configurations At Supersonic Mach Numbers
Usta, Engin; Kıvanç, Arslan; Tuncer, İsmail Hakkı (2015-09-10)
In this study a neural network based method is developed for the prediction of separation characteristics of external store weapons carried under aircraft wings. The method is based on an artificial neural network trained by high fidelity unsteady flow solutions. The unsteady flow solutions as the store separates from the carriage and the resulting six degrees of freedom motion of the store are computed conditions by a commercial flow solver for various flight conditions. The trajectory of the store and the...
AERODYNAMIC ANALYSIS OF SUPERSONIC FLOW OVER A SIMPLE AIRCRAFT GEOMETRY BY USING CST AND PANEL METHODS
Uğur, Levent; Turan, Sena; Gedik, Ramazan Kürşat; Adam, Ali Ata; Sezer Uzol, Nilay; Ertem, Sercan; Ayan, Erdem (2021-09-10)
In this paper, the aerodynamic properties of a selected aircraft geometry are calculated in supersonic flow condition using PANAIR. PANAIR is an open-source high-order panel method solver for irrotational and inviscid flows and it is more efficient than higher fidelity CFD analyses for the preliminary design process since it is faster and easier to use. A batch of supersonic analyses is completed for different wing/body configurations for the selected aircraft geometry and with various panel g...
Aerodynamic Modelling and Analysis of a Novel Mechanism for Chord and Camber Morphing Wing
Şahin, Harun Levent; Çaklr, Bora Orçun; Yaman, Yavuz (2018-06-22)
This paper presents the aerodynamic modelling and analysis of surfaces created by a novel deployable mechanism, which is composed of a four-bar linkage and a scissor-structural mechanism (SSM) which contains several scissor-like elements (SLEs). With the help of that mechanism, which is located inside the trailing portion of wing section, continuous adjustment of the airfoil is possible. In order to highlight the advantageous aerodynamic characteristics of newly created airfoil geometries via proposed SSM, ...
Citation Formats
H. Erhan, “Aerodynamic analysis of fighter aircraft F-16 with external stores,” M.S. - Master of Science, Middle East Technical University, 2003.